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An Earth-mass planet in a time of COVID-19: KMT-2020-BLG-0414Lb

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© 2021 National Astronomical Observatories, CAS and IOP Publishing Ltd.
, , Citation Weicheng Zang et al 2021 Res. Astron. Astrophys. 21 239 DOI 10.1088/1674-4527/21/9/239

1674-4527/21/9/239

Abstract

We report the discovery of KMT-2020-BLG-0414Lb, with a planet-to-host mass ratio q2 = 0.9–1.2 × 10−5 = 3–4 ⊕ at 1σ, which is the lowest mass-ratio microlensing planet to date. Together with two other recent discoveries (4 ≲ q/q ≲ 6), it fills out the previous empty sector at the bottom of the triangular (log s, log q) diagram, where s is the planet-host separation in units of the angular Einstein radius θE. Hence, these discoveries call into question the existence, or at least the strength, of the break in the mass-ratio function that was previously suggested to account for the paucity of very low-q planets. Due to the extreme magnification of the event, Amax ∼ 1450 for the underlying single-lens event, its light curve revealed a second companion with q3 ∼ 0.05 and |log s3| ∼ 1, i.e., a factor ∼ 10 closer to or farther from the host in projection. The measurements of the microlens parallax πE and the angular Einstein radius θE allow estimates of the host, planet and second companion masses, (M1, M2, M3) ∼ (0.3 M, 1.0 M, 17 MJ), the planet and second companion projected separations, (a⊥,2, a⊥,3) ∼ (1.5, 0.15 or 15) au, and system distance DL ∼ 1 kpc. The lens could account for most or all of the blended light (I ∼ 19.3) and so can be studied immediately with high-resolution photometric and spectroscopic observations that can further clarify the nature of the system. The planet was found as part of a new program of high-cadence follow-up observations of high-magnification events. The detection of this planet, despite the considerable difficulties imposed by COVID-19 (two KMT sites and OGLE were shut down), illustrates the potential utility of this program.

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1. Introduction

It has long been known that intensive monitoring of high-magnification microlensing events is sensitive to planets of one-to-few Earth/Sun mass ratio, q = 3 × 10−6, planets. Dong et al. (2006) showed that the Amax ∼ 3000 event OGLE-2004-BLG-343 would have had such sensitivity had it been observed over peak (see their fig. 9). Yee et al. (2009) demonstrated such sensitivity for the actual data covering the peak of the Amax ∼ 1600 event OGLE-2008-BLG-279 (see their fig. 7). In both cases (and, indeed, for high magnification events in general, Gaudi et al. 2002; Gould et al. 2010), the sensitivity diagrams have a triangular appearance that is symmetric in log s about the origin. That is, the contour limits meet at s = 1, where s is the planet-host separation in units of the Einstein radius θE. Hence, the limiting sensitivity in q is via a so-called "resonant caustic". For s ≫ 1, the caustic structure consists of a small quadrilateral caustic near the host and a larger quadrilateral caustic near the planet. For s ≪ 1, it consists of a similar small quadrilateral caustic near the host and two triangular caustics located on the opposite side of the planet. For s ∼ 1, these two sets of caustics merge into a relatively large 6-sided "resonant" caustic, which is what makes the detection feasible at the very limit of sensitivity 1 .

Neither of the above two events yielded any planet detection, but Udalski et al. (2018) did find a resonant-caustic planet in OGLE-2017-BLG-1434 (Amax ∼ 23 for the underlying single-lens event). While its mass ratio was q ∼ 5.7 × 10−5 (i.e., q ∼ 19 q), Udalski et al. (2018) showed that a planet with exactly the same characteristics, but 30 times less massive, would have been detected (see their fig. 4).

Nevertheless, in spite of the recognized theoretical possibility of such few-q planet detections, no planet with mass ratio below that of the Uranus/Sun mass ratio q ∼ 15 q was actually detected prior to 2018 2 . This failure gave rise to several different suggestions of a paucity in low mass-ratio planets. Suzuki et al. (2016) argued for a "break" in the mass-ratio function at qbr ∼ 57 q based on a statistically well-defined sample of planets detected from Microlensing Observations in Astrophysics (MOA)-discovered microlensing events. Jung et al. (2019) claimed a "break", or possibly a "pile-up", at q ∼ 19 q based on the ensemble of planets with q < 3 × 10−4. Udalski et al. (2018) followed a new "V/Vmax" method to show that if planets with q < 10−4 were modeled as a power-law distribution in q, then the distribution was rising toward higher q, seemingly confirming the Suzuki et al. (2016) "break".

However, in 2018 and 2019, three planets were discovered with q below the previous record, and hence below the level of the conjectured "break" or "pile-up": KMT-2018-BLG-0029Lb (q ∼ 1.8 × 10−5, Gould et al. 2020), KMT-2019-BLG-0842Lb (q ∼ 4.1 × 10−5, Jung et al. 2020) and OGLE-2019-BLG-0960Lb (q ∼ 1.4 × 10−5, Yee et al. 2021). All three were detected via resonant caustics at or near the peak of moderately high magnification events, with |s – 1|∼(0.000,0.017,0.003 or 0.029). Moreover, Yee et al. (2021) reported that the recent discoveries of KMT-2018-BLG-0029Lb and OGLE-2019-BLG-0960Lb populate the previously-vacant lower region of the (log s,log q) diagram. See their figure 11. It is therefore clear that the well-established sensitivity to qq depends primarily on relatively rare (i.e., high-magnification) microlensing events generated by relatively rare resonant lens configurations. Therefore, it is possible that the previous paucity of planets near the detection limit was more a product of the difficulty of detection than the intrinsic rarity of the population.

In this context, it is notable that over the last 10 years, microlensing planet searches have moved away from their previous focus on high-magnification events, which is one of the two "rare elements" just described for probing the low-q population. Prior to the inauguration of the wide-field-camera OGLE-IV survey (Udalski et al. 2015), substantial effort was expended, particularly by the Microlensing Follow Up Network (FUN), to find high-magnification events, and then to focus intensive observations over the peak (Gould et al. 2010). As a result, the projected spatial distribution of planetary events was drawn roughly uniformly from the OGLE-III and MOAII surveys. See the blue circles in figure 8 of Ryu et al. (2020a). That is, the surveys were able to detect events, more or less regardless of cadence, but were much less able to detect planets on their own, again regardless of cadence. Hence, planet-yielding events were unaffected by survey cadence. However, with the layered approach (higher cadence in more productive fields) made possible by the introduction of the larger-format OGLE-IV camera, planet searches came to rely more on survey data, so that planetary discoveries became more concentrated on highcadence regions. See green and yellow points in the same diagram. This remained so with the advent of the still larger-format KMTNet (Kim et al. 2016) survey (magenta and black points).

Beginning in 2016, KMTNet continuously monitored ∼ 97 deg2 area of sky toward the Galactic bulge field from three 1.6 m telescopes equipped with 4 deg2 field of view (FOV) cameras at CTIO in Chile, SAAO in South Africa and SSO in Australia. In fact, KMTNet's three-observatory system is capable of detecting very low-q planets in its highest cadence, Γ = 4 hr−1 fields, as was proved by the case of KMT-2019-BLG-0842Lb. The substantially lower-q planet KMT-2018-BLG-0029Lb was discovered in KMT-only observations of a Γ = 1 hr−1 field. For the lowest-q planet OGLE-2019-BLG-0960Lb, although the planetary signal was first recognized by the μFUN CT13 data and was most clearly delineated by the μFUN Kumeu data, the detection would probably have been regarded as secure using the low-cadence survey observations (ΓKMT ∼ 0.4 hr−1, three sites; ΓOGLE = 0.17 hr−1, one site; ΓMOA = 0.6 hr−1, one site).

An additional notable feature of these detections is that the magnification of the underlying 1L1S event at the time of the planetary anomaly was modest (Aanom ∼ 37 for KMT-2018-BLG-0029Lb, Aanom ∼ 22 for KMT-2019-BLG-0842Lb and Aanom ∼ 45 for OGLE-2019-BLG-0960Lb), although Amax ∼ 160 for the latter two cases. The source trajectory was "oblique", i.e., close to parallel to the long axis of the resonant caustic, with α = 8.3° and α = 15.5° for KMT-2019-BLG-0842Lb and OGLE-2019-BLG-0960Lb, respectively. While such oblique trajectories are relatively rare, they can enhance detection efficiency by "stretching out" anomalies. Moreover, Yee et al. (2021) found that sensitivity to very low-q planets can be maximized by intensively monitoring events whenever they were magnified by a factor A > 10 (see also Abe et al. 2013). In order to probe the very low-q planets, KMTNet together with the Las Cumbres Observatory global network (LCOGT) & μFUN Follow-up Team developed a program for focusing on observations and analysis of A ≳ 20 events located in KMTNet Γ ≤ 1 hr−1 fields.

However, with the advent of COVID-19, two of KMT's three observatories were shut down, leaving only KMT's Australia telescope as operational. Hence, the conditions became much more similar to those of the first decade of this century, when microlensing alerts came primarily from the OGLE-III survey, and planets were primarily discovered by follow-up observations of these single-site alerts, as well as some non-overlapping alerts from MOA. Of course, there were some differences. In particular, KMT has a much larger format camera than OGLE-III, and so it operates at substantially higher cadence. However, KMTA also has the worst conditions of KMT's three observatories, and so is inferior to OGLE-III in terms of both weather interruptions and photometric precision.

It was the specific orientation of this program, i.e., follow-up observations of A ≳ 20 events, that led to the discovery of KMT-2020-BLG-0414Lb, the lowest mass-ratio microlensing planet discovered to date, q2 ∼ 10−5. Due to the extreme magnification of the event, Amax ∼ 1450 for the underlying single-lens event, and high-cadence observations by MOA over the peak, a second companion was also detected, with q3 ∼ 0.05.

2. Observations

KMT-2020-BLG-0414 occurred at equatorial coordinates (α, δ)J2000 = (18:07:39.60, –28:29:06.8), corresponding to Galactic coordinates (,b) = (2.82, –3.95). It was announced as a "probable microlensing" event by the KMTNet Alert-Finder system (Kim et al. 2018) on 2020 June 1, about 40 days before peak, when the event was manifested as an I ∼ 18.7 difference star. As mentioned in Section 1, by this date, KMTC and KMTS had been closed down for more than two months due to COVID-19. Hence, only KMTA data contributed to the alert and to subsequent monitoring of the event. The event lies in the KMNTet BLG32 field, which has a cadence of Γ = 0.4 hr−1, with every tenth I-band observation complemented by one in the V band for the source color measurements 3 .

The event was independently identified by the MOA (Sumi et al. 2016) Collaboration as MOA-2020-BLG-109 on 2020 June 20 (Bond et al. 2001). MOA observations are carried out with a 1.8 m telescope at the Mt. John University Observatory in New Zealand, which is equipped with a 2.2 square degree camera. The nominal cadence for this field was Γ = 1.2 hr−1 by an MOA-Red filter (which is similar to the sum of the standard Cousins R- and I-band filters), and observations with the MOA V filter (Bessell V-band) were taken once every clear night. Earlier in the season, the MOA survey had also been closed for COVID-19 for almost 100 days, but it had re-opened 28 days before peak. Hence, the COVID-19 hiatus had very little effect on its observations of this event.

Due to the poor seeing at KMTA and the rough real-time difference image analysis (DIA) photometry, the KMTNet Alert-Finder system found that a catalog star at (α, δ)J2000 = (18:07:39.60,–28:29:05.50) had the strongest signal and identified it as the preliminary source position of KMT-2020-BLG-0414. This catalog star is about 1.3'' away from the true position of the source. As a result, the real-time on-line photometry was relatively noisy. Nevertheless, at UT 17:34 on 2020 July 7 (HJD' = 9038.23, HJD' = HJD – 2450000), the LCOGT & μFUN Follow-up Team found that this event had magnification Anow > 10 based on the two KMTA points at HJD' ∼ 9038 and could peak at a high magnification 2–3 days later 4 . Thus, high-cadence follow-up observations were immediately scheduled by LCOGT and Observatorio do Pico dos Dias (OPD) in Brazil (a μFUN site). The LCOGT conducted observations from its 1.0 m telescopes located at SAAO (LCOS), SSO (LCOA) and McDonald (LCOM), with the Sloan Digital Sky Survey (SDSS)-i' filter. Observations by OPD were taken from its 0.6 m (OPD06) and 1.6 m (OPD16) telescopes with the I filter. At UT 05:58 on 2020 July 10 (HJD' = 9040.75), the LCOGT & μFUN Follow-up Team identified that this event was currently undergoing an anomaly and would peak at a very high magnification soon, based on the real-time LCOGT and MOA data. Noting that SSO was predicted to be rainy that night, the team issued an alert to the MOA collaboration. MOA responded to the alert and densely observed this event 60 times over the peak. Due to the very high brightness, the MOA observer decreased the exposure time from 60 s to 5.2 s over the peak. We carefully inspected these 60 MOA images and excluded 19 data points from the analysis due to saturation or bad seeing. At UT 13:53 on 2020 July 10 (HJD' = 9041.08), the LCOGT & μFUN Follow-up Team also issued an alert to all μFUN observers. As a result, the 0.3 m Perth Exoplanet Survey Telescope (PEST) in Australia and the 0.4 m Possum Observatory (Possum) in New Zealand responded to the alert and took intensive observations without a filter. Finally, the event was also observed by the 3.6 m Canada-France-Hawaii Telescope (CFHT) with the SDSS-i' filter.

For the light curve analysis, the KMTNet, MOA, CFHT and LCOGT data were reduced using custom implementations of the DIA technique (Tomaney & Crotts 1996; Alard & Lupton 1998): pySIS (Albrow et al. 2009) for the KMTNet data, Bond et al. (2001) for the MOA data and ISIS (Alard & Lupton 1998; Alard 2000; Zang et al. 2018) for the CFHT and LCOGT data. The OPD, PEST and Possum data were reduced employing DoPHOT (Schechter et al. 1993). On the OPD16 images, the target was affected by a bleed trail from a saturated star, resulting in some systematics. We therefore do not include OPD16 data in the analysis. The I-band magnitude of the KMTA light curve has been calibrated to the standard I-band magnitude. For the source color measurements, we utilize the MOA V-band data, while KMTA V-band data are not used due to poor seeing. The errors from photometric measurements for each data set i were renormalized applying the formula ${\sigma }_{i}^{\prime}={k}_{i}\sqrt{{\sigma }_{i}^{2}+{e}_{i,{\rm{\min }}}^{2}}$, where σi and ${\sigma }_{i}^{\prime}$ are original errors from the photometry pipelines and renormalized error bars in magnitudes respectively, and ki and ei, min are rescaling factors. We obtained the rescaling factors following the procedure of Yee et al. (2012), which enables χ2/dof for each data set to become unity. We derived the rescaling factors using the binary lens (2L1S) and triple lens (3L1S) models, in order to understand how the event would have been interpreted in the absence of MOA data on the peak. The data considered in the analysis, together with corresponding data reduction method and rescaling factors are summarized in Table 1.

Table 1. Data Used in the Analysis with Corresponding Data Reduction Method and Rescaling Factors

CollaborationSiteFilterCoverage (HJD') Ndata Reduction Method(k, emin) for 2L1S(k, emin) for 3L1S
KMTNetSSO I 8900.3 – 9139.0139pySIS 1 (1.23, 0.010)(1.11, 0.020)
KMTNetSSO V 8931.2 – 9130.921pyDIA 2  
MOA Red9024.2 – 9145.9240Bond et al. (2001)(1.74, 0.006)(1.35, 0.020)
MOA  V 9022.0 – 9112.922Bond et al. (2001) 
LCOGTSSO i 9038.9 – 9047.253ISIS 2 (1.08, 0.002)(0.35, 0.010)
LCOGTSAAO i 9038.3 – 9055.5107ISIS(1.31, 0.001)(1.05, 0.005)
LCOGTMcDonald i 9040.7 – 9046.762ISIS(1.03, 0.003)(1.10, 0.005)
CFHT  i 9041.9 – 9051.923ISIS(3.25, 0.000)(1.10, 0.020)
μFUNOPD06 I 9040.4 – 9045.7105 DoPHOT 3 (1.15, 0.002)(1.33, 0.000)
μFUNOPD16 I 9038.5 – 9049.6861 DoPHOT  
μFUNPESTunfiltered9042.2 – 9051.098 DoPHOT (0.82, 0.016)(0.71, 0.020)
μFUNPossumunfiltered9041.8 – 9052.0143 DoPHOT (0.81, 0.027)(0.87. 0.020)

HJD' = HJD – 2450000. MOA V-band data are only used to determine the source color. KMT SSO V-band data are not utilized due to poor seeing. OPD16 data are not included in the analysis due to bleeding from a bright star. For the MOA data, the 41 points on the peak (9040.78 < HJD' < 9041.20) are excluded in the 2L1S analysis. 1Albrow et al. (2009). 2MichaelDAlbrow/pyDIA: Initial Release on Github, doi:10.5281/zenodo.268049. 3Alard & Lupton (1998); Alard (2000); Zang et al. (2018). 4Schechter et al. (1993).

3. 2L1S Analysis

Figure 1 depicts the observed light curve of KMT-2020-BLG-0414. Although the light curve can be regarded as a "single peak" in the sense that it monotonically rises and then falls, its significantly asymmetric shape cannot be fitted by a single-lens single-source (1L1S) model. A 1L1S model is usually described by three Paczyński (1986) parameters (t0, u0, τE ), i.e., the time of closest lens-source approach, the impact parameter scaled to θE and the Einstein crossing time,

Equation (1)

where ML is the mass of the lens and (πrel, μ rel) are the lens-source relative (parallax, proper motion). In the present case, we also consider finite-source effects (Gould 1994; Witt & Mao 1994; Nemiroff & Wickramasinghe 1994), which which occur when the source passes close to singular structures in the magnification pattern. This requires a fourth parameter ρ = θ* / θE, where θ* is the angular radius of the source.

Fig. 1

Fig. 1 Light curve of KMT-2020-BLG-0414. with lensing models. The circles with different colors are the observed data points for different data sets. The black solid line is the best-fit 3L1S model incorporating all the data, the cyan solid line is the best-fit 2L1S model excluding the MOA data on the peak and the black dashed line is the 1L1S model derived using the same (t0, u0, τE, ρ) as the best-fit 3L1S model. The middle and bottom panels feature a close-up of the main perturbations from the q ∼ 10−5 planet and the third body (q ∼ 0.05), respectively.

Standard image

As we will show in Section 4, the full light curve cannot be explained by a 2L1S model, and in fact requires 3L1S. However, if we exclude the MOA data on the peak (9040.78 < HJD' < 9041.20, the only data set to cover the peak), then the remaining data are quite well fit by a 2L1S model. We therefore begin by analyzing this restricted (non-MOA-peak) data set. We are motivated by two considerations. First, and most importantly, 3L1S models often "factor" into two 2L1S models (Han 2005; Gaudi et al. 2008; Gould et al. 2014; Han et al. 2013, 2017, 2019a). In particular, the 3L1S caustic is often very nearly the superposition of the two 2L1S caustics. In such cases, one can often exclude the data from the neighborhood of the anomaly from the "second" 2L1S model in order to accurately determine the parameters of the "first" 2L1S model. In these cases, the "first" 2L1S model provides a powerful basis for finding the full 3L1S model, by one of several techniques. This proves to be the case for KMT-2020-BLG-0414.. Second, it is of independent scientific interest to understand how the event would have been interpreted and check the so-called "higher-order effects" in the absence of MOA data on the peak. For example, MOA could have been clouded out on the night of the peak (as was KMTA). The analysis would have led to a report of a single low-mass-ratio planet and a lens that is much brighter than the blended light. The comparison of this reconstructed "report" with the full model can inform our understanding of other 2L1S events with incomplete light-curve coverage.

Therefore, for the remainder of this section, we will exclude the MOA data on the peak. These data will then be incorporated in Section 4.

3.1. Static Binary Lens Model

The 2L1S model requires three additional parameters e(s, q, α), which are respectively the separation of the two lens bodies scaled to θE, the mass ratio between these bodies and the angle of the source trajectory relative to the binary axis. For modeling, we use the advanced contour integration code (Bozza 2010; Bozza et al. 2018), VBBinaryLensing 5 . We initially carry out sparse grid searches for the parameters (log s, log q, α). The grid consists of 21 values equally spaced between –1.0 ≤ log s ≤ 1.0, 20 values equally spaced between 0° ≤ α < 360° and 61 values equally spaced between –6.0 ≤ log q ≤ 0.0. For each set of (log s, log q, α), we find the minimum χ2 by Markov chain Monte Carlo (MCMC) χ2 minimization utilizing the emcee ensemble sampler (Foreman-Mackey et al. 2013), with fixed log q, log s and free t0, u0, τE, ρ, α. We identify one local minimum at (log s,log q) ≃ (0.0, –5.1), similar to the case of Yee et al. (2021). We thus conduct a similar dense grid search as Yee et al. (2021) that consists of 51 values equally spaced between –0.02 ≤ log s ≤ 0.03 and 41 values equally spaced between –6.0 ≤ log q leq –4.0. Often, such a grid search yields two local minima at s > 1 and s < 1 (e.g., Jung et al. 2020; Yee et al. 2021), which must then be individually further explored and compared. However, in the present case, there is only one local minimum at s < 1, while the s > 1 model is disfavored by Δχ2 > 900. We refine this minimum by allowing all parameters to vary. The parameters with their 68% uncertainty range from the MCMC are displayed in Table 2, and the fit and residuals are depicted in Figure 1. The very low mass ratio q ∼ 10−5 indicates that the companion is a very-low-mass planet.

Table 2. Parameters for 2L1S Model

ParametersStatic (non-parallax)ParallaxParallax + Orbital Motion
   u0 > 0 u0 < 0 u0 > 0 u0 < 0
χ2/dof 948.6/904902.8/902921.0/902900.4/900917.4/900
t0 (HJD')9041.05909041.05969041.05619041.05949041.0562
 0.00090.00100.00110.00110.0012
u0 (10−3)0.1250.153–0.1560.160–0.170
 0.0140.0150.0160.0180.019
τE (d)102.993.591.695.995.7
 6.34.94.96.26.1
s 0.995910.995420.995210.995040.99454
 0.000250.000250.000280.000520.00058
q (10−5)0.690.951.011.071.24
 0.130.150.170.220.25
α (rad)0.01770.0199–0.02050.0214–0.0232
 0.00110.00110.00120.00220.0024
ρ (10−4)4.105.105.395.295.80
 0.530.560.620.630.66
πE, N ...0.0350.0800.0350.076
 ...0.0160.0220.0160.022
πE, E ...0.2260.1530.2250.147
 ...0.0410.0380.0410.038
ds/dt (yr−1).........0.1960.345
 .........0.2510.279
/dt (yr−1)..........0.017–0.021
 ..........0.059–0.061
IS 19.20919.10419.07519.13219.126
 0.0700.0590.0600.0720.072

HJD' = HJD – 2450000. Uncertainties are given in the second line for each parameter. t0 represents the time of closest approach of the source to the lens mass center. u0 is the closest distance of the source to the lens mass center.

3.2. Microlens Parallax Model

Even without detailed analysis, the results for the static model, that are listed in Table 2, imply a large (and so potentially measurable) microlens parallax (Gould 1992, 2000),

Equation (2)

According to θ* and the blended light in Section 5, θE = θ*/ρ ≥ 1.68 mas and the lens light IL ≥ 18.9 at 3σ level. The two limits correspond roughly to an M ∼ 0.5 M at a distance of 1.2 kpc. Thus, we can expect 6

Equation (3)

Moreover, given the long Einstein timescale, θE ∼ 103 d, the projected velocity on the observer plane, $\tilde{v}\equiv {\rm{au}}/({\pi }_{E}{t}_{E})\,\le 42\,{\rm{km}}\,{{\rm{s}}}^{-1}$ is close to the changes of Earth's velocity over the course of the event, taking account of which could impact other parameters as well.

Therefore, it is essential to include microlens-parallax effects in the fit. We fit the annual microlens-parallax effect by introducing two additional parameters πE,N and πE,E, the north and east components of π E in equatorial coordinates (Gould 2004). We also fit u0 > 0 and u0 < 0 models to consider the "ecliptic degeneracy" (Jiang et al. 2004; Poindexter et al. 2005). Table 2 lists the results of fitting the light curve with the microlens parallax effect. Because the annual parallax effect can be degenerate with the effects of lens orbital motion (Batista et al. 2011; Skowron et al. 2011), we also introduce two linearized parameters (ds/dt, /dt), the instantaneous changes in the separation and orientation of the two lens components defined at t0. We restrict the MCMC trials to β < 0.8, where β is the ratio of projected kinetic to potential energy (Dong et al. 2009)

Equation (4)

where we adopt the source parallax πs = 0.128 mas based on the mean distance to clump giant stars in this direction (Nataf et al. 2013). See Table 2 for the results. We find that the addition of lens orbital motion effect provides improvements of Δχ2 = 2.4 and 5.4 for the u0 > 0 and u0 < 0 solution, respectively, and πE is basically the same compared to the "parallax" model.

Although the angular Einstein radius θE estimated from the parallax modeling is smaller than the value from the static model, the resulting parallax for 2L1S is still strongly inconsistent with the constraint of the blended light at about 3σ. We will further discuss the implication of the 2L1S results in Section 6.1.

3.3. Binary-Source (1L2S) Model

In some cases, planetary (2L1S) light curves can be imitated by binary-source (1L2S) events (Gaudi 1998). We do not expect that this will be the case for KMT-2020-BLG-0414. because the planetary anomaly is mainly characterized by sharp changes in slope, rather than a smooth short-lived bump. Nevertheless, as a matter of due diligence, we search for such models including both microlens-parallax and microlens-xarallap effects (Griest & Hu 1992; Han & Gould 1997; Poindexter et al. 2005). We find that while the introduction of a second source yields a huge improvement with respect to the 1L1S model with Δχ2 = χ2(1L1S) – χ2(1L2S) > 10 000, the 1L2S model still does not compete with the 2L1S model with Δχ2 = χ2(1L2S) – χ2(2L1S) > 400.

4. 3L1S Analysis

While the 2L1S models described in Section 3 fit the non-MOA-peak data very well, they completely fail to explain the features of the MOA data in the peak region. Moreover, a 2L1S grid search that includes all the data fails to return any model that even approximately traces the data over the peak. See Figure 1. We therefore conduct a 3L1S grid search. Relative to static 2L1S models, 3L1S models have three additional parameters, (s3, q3, ψ). These are, respectively, the normalized separation of the third body from the primary, the mass ratio of the third body to the primary and the angle of the second from the third body, as seen from the primary. Note that, to avoid confusion, we rename (s, q) → (s2, q2).

4.1. 3L1S Static Models

We begin by conducting a grid search for static 3L1S solutions that is analogous to the one carried out previously for 2L1S solutions, but is substantially more computationally intensive. In a grid search (whether 2L1S or 3L1S), the lens geometry is held fixed at each grid point. However, for 2L1S, the geometry is specified by just two parameters, (s2, q2), whereas for 3L1S, five geometric parameters are required, (s2, q2, s3, q3, ψ). To reduce the grid of geometries from five to three dimensions, we consider a (70 × 70 × 180) grid in (s3, q3, ψ). We hold (s2, q2) fixed at the best-fit 2L1S model. We seed the remaining five parameters, (t0, u0, θE, ρ, α), at the best-fit 2L1S model, and we then allow these to vary. We initially consider only close models for the third body, i.e., s3 < 1. For the grid-search phase, which relies on fixed geometries, we apply the map-making technique of Dong et al. (2006) to evaluate the magnifications. This grid search yields only one local region of candidate solutions.

We then seed an additional MCMC with the best grid point from this region and allow all 10 parameters to vary. Because the geometry now varies with each step in the MCMC, we apply the adaptive-image inverse-ray-shooting technique to evaluate the magnifications. The resulting parameters are shown in Table 3, and the model light curve is compared to the data in Figure 1. The corresponding caustic structure in the upper panel of Figure 2 demonstrates that KMT-2020-BLG-0414. is a classic case of "caustic factorization". The caustic is nearly the superposition of two well-known caustic types: a large resonant caustic associated with the planet, and a smaller, nearly Chang-Refsdal (Chang & Refsdal 1979), caustic associated with the third body. As is often the case, the two caustic structures "interact" and become intertwined where they overlap. Because of the caustic factors and q3 ≪ 1, it is straightforward to guess the alternate wide (s3 > 1) solution according to the prescription of Griest & Safizadeh (1998): ${s}_{3}\to {s}_{3}^{-1}$. We seed this guess into an MCMC to yield the alternate wide solution, whose parameters are given in Table 3 and whose geometry is displayed in the lower panel of Figure 2. The most striking difference between the 3L1S close and wide solutions is that s2, close = 0.99914 ± 0.00011, while s2, wide = 0.96882 ± 0.00018, which appears to be a "100σ" difference. We address this issue in Appendix A.

Fig. 2

Fig. 2 Geometries of the 3L1S Close (upper panel) and Wide (lower panel) models. In each panel, the red dashed line represents the caustic structure, the black solid line is the trajectory of the source and the arrow indicates the direction of the source motion. The 3L1S caustic is nearly the superposition of a large six-sided "resonant" caustic associated with the q ∼ 10−5 planet and a small quadrilateral caustic associated with the third body (q ∼ 0.05).

Standard image

Table 3. Parameters for 3L1S Static and Parallax Model

ParametersStatic (non-parallax)Parallax
 CloseWideClose u0 > 0Close u0 < 0Wide u0 > 0Wide u0 < 0
χ2/dof 1093.8/9421094.7/942944.6/940956.2/940964.8/940962.1/940
t0 (HJD')9041.03759041.03629041.03609041.03599041.03659041.0357
 0.00090.00060.00120.00090.00100.0010
u0 (10−3)0.7190.7190.688–0.6840.747–0.706
 0.0150.0070.0190.0060.0130.008
τE (d)91.390.394.695.388.393.0
 1.11.12.10.71.20.9
s2 0.999140.968820.998270.998320.968490.97315
 0.000110.000180.000190.000140.000530.00023
x2 0.995220.994940.995110.995210.994530.99495
 0.000120.000120.000190.000110.000180.00014
q2 (10−5)1.201.261.131.121.411.23
 0.050.040.080.020.060.03
α (rad)0.02570.02180.0251–0.02530.0230–0.0224
 0.00050.00020.00060.00020.00040.0003
s3 0.095510.46330.10960.110810.32049.6413
 0.00010.00020.00340.00260.04570.0366
q3 0.05840.05460.04040.03950.05450.0453
 0.00110.00020.00290.00210.00110.0005
ψ (rad)–0.729–0.746–0.7300.733–0.7300.741
 0.0080.0050.0140.0100.0130.011
ρ (10−4)5.605.865.785.726.696.10
 0.150.130.270.080.180.12
πE, N ......0.0570.321–0.0110.343
 ......0.0420.0350.0350.045
πE, E ......0.4670.1960.3660.222
 ......0.0730.0590.0560.067
IS 19.08219.04019.12319.12519.01019.073
 0.0140.0140.0250.0070.0150.009

HJD' = HJD – 2450000. Uncertainties are given in the second line for each parameter. t0 represents the time of closest approach of the source to the lens mass center. u0 is the closest distance of the source to the lens mass center. x2 is a derived quantity and is not fitted independently. See Appendix A for the definition of x2.

Table 4. Parameters for 3L1S Model with Parallax and Planet Orbital Motion

ParameterClose u0 > 0Close u0 < 0Wide u0 > 0Wide u0 < 0
χ2/dof 939.7/938938.0/938944.8/938939.5/938
t0 (HJD')9041.03699041.03629041.03579041.0355
 0.00100.00120.00120.0011
u0 (10−3)0.652–0.6880.693–0.720
 0.0200.0110.0170.012
τE (d)99.494.493.890.4
 2.41.12.01.5
s2 0.999250.998960.972020.96835
 0.000260.000350.001730.00060
x2 0.995370.995210.995030.99496
 0.000230.000110.000260.00027
q2 (10−5)1.011.131.141.21
 0.110.060.070.06
α (rad)0.0255-0.02690.0222–0.0233
 0.00100.00050.00060.0005
s3 0.08950.09409.971310.5031
 0.00400.00510.41970.0607
q3 0.06160.05780.04760.0557
 0.00380.00710.00380.0013
ψ (rad)–0.7260.731–0.7370.740
 0.0130.0130.0150.013
ρ (10−4)5.335.785.926.20
 0.300.160.230.17
πE, N 0.389–0.3450.480–0.552
 0.1540.1200.1520.203
πE, E 0.1730.6690.2200.809
 0.1350.1050.1210.140
ds/dt (yr−1)0.008–0.022-0.034–0.091
 0.0540.0550.0620.054
/dt (yr−1)0.466–0.8480.496–1.054
 0.1690.1370.1810.212
β 0.0420.0580.0350.055
 0.0180.0060.0140.005
IS 19.17319.12119.08419.042
 0.0260.0130.0210.017

HJD' = HJD – 2450000. Uncertainties are given in the second line for each parameter. t0 represents the time of closest approach of the source to the lens mass center. u0 is the closest distance of the source to the lens mass center. β and x2 are derived quantities and are not fitted independently. See Eq. (4) and Appendix A for the definitions of β and x2, respectively.

4.2. 3L1S Parallax-only Models

As discussed in Section 3.2, the microlens-parallax parameters π E (Eq. (2)) can be degenerate with the orbital-motion parameters γ (Eq. (4)). Hence, both should be considered together. However, as in that section, we proceed step-by-step, in part due to the increasing computational load as more parameters are introduced, and therefore the importance of understanding which are really necessary.

When only π E is added to the 3L1S static model, there are 12 parameters. As was the case for 2L1S, adding parallax to the fit results in doubling the number of solutions, i.e., there is a ± u0 pair of solutions for each of the close and wide solutions found in Section 4.1. Hence there are four solutions altogether. The resulting parameters and χ2 values are given in Table 3. It is found that including parallax significantly improves the fit by Δχ2 > 130. The wide solutions are disfavored by Δχ2 > 17. Between the two close solutions, the u0 > 0 solution is significantly favored by Δχ2 ∼ 12. We note that the magnitude of π E for 3L1S is substantially larger than the value estimated from the 2L1S modeling regardless of the lens-orbital effect. Figure 3 shows the cumulative distribution of Δχ2 = χ2(static) – χ2(parallax) for the four solutions. Overall, Δχ2 grows steadily over time, giving credence to the parallax measurement. An important feature of this diagram is that the contribution to Δχ2 during the short time interval starting from one day before the peak and ending two days after the peak is about 40% of the total Δχ2. By contrast, one normally expects the parallax signal to be dominated by the wings of the light curve. This time interval is essentially the duration of contact with the planetary caustic, in particular as the source "rides the caustic" for two days after the peak. This gives a plausible explanation for the sensitivity of π E to the near-peak region of the light curve. Hence, it is essential to include orbital motion.

Fig. 3

Fig. 3 Cumulative distribution of $\Delta {\chi }^{2}={\chi }_{{\rm{static}}}^{2}-{\chi }_{{\rm{parallax}}}^{2}$ between the four 3L1S parallax solutions and the two 3L1S static solutions. Overall, Δχ2 grows steadily over time and does so steeply from one day before peak until two days after peak, when the source touches the planetary caustic. The upper panel features the best-fit 3L1S parallax model.

Standard image

4.3. 3L1S Parallax and Planet Orbital Motion

We now include both π E and γ for the planet in the 3L1S fit, for a total of 14 chain parameters. We display the parameters of this fit in Table 3. It is found that including planet orbital motion significantly changes π E in both magnitude and direction, and |πE| of the u0 < 0 solution is ∼ 1.8 times greater than that of the u0 > 0 solution. The close u0 < 0 solution has the best fit to the observed data, while other solutions are only disfavored by Δχ2 < 7. Thus, we cannot exclude any solution from the light-curve analysis. The ratio β of projected kinetic to potential energy is measured well, and all of the solutions have β < 0.1 at 3σ. This relatively low value of the ratio suggests that the planet and the host may be aligned along the line of sight.

4.4. Possible Orbital Motion of the Third Body

The third body (with a brown-dwarf-like mass ratio q3 ∼ 0.05) must also undergo orbital motion. In the wide solutions, the period would be of order 100 years, implying that orbital motion of the third body would not affect the lensing light curve. For the close solutions, the period would be of order 50 days, and thus its orbital motion could affect the light curve. Nevertheless, we do not attempt to model orbital motion of the third body for several reasons. First, the duration of its pronounced perturbation (∼ 0.3 days over the peak) is 10 times shorter than for the duration of the planetary signal, and its impact on the light curve is quadratic in the duration. Second, if there were clear prospects of a scientifically important result, such work would be warranted, but there are no such prospects (see Sect. 5.4). Finally, the results of 3L1S parallax + planet orbital motion required about two weeks of computations with 400 processors. The already prodigious use of computer time (which scales ∝ (n/2)! where n is the number of chain parameters) would increase by a factor eight. We therefore decline to pursue this aspect of the problem.

5. Physical Parameters

Normally, if the angular Einstein radius θE and the microlens parallax πE are measured well, one can simply determine the lens total mass ML and the lens distance DL by (Gould 1992, 2000)

Equation (5)

However, in the present case, the lens system is very close (DL ∼ 1 kpc), and the large symmetric errors of πE can lead to an asymmetric distribution in inferred lens distance. Hence, we conduct a Bayesian analysis to estimate the lens physical parameters in Section 5.3. Before doing so, we estimate θ* by a color-magnitude diagram (CMD) analysis (Yoo et al. 2004) in Section 5.1, in order to estimate the angular Einstein radius by θE = θ*/ρ. We also study the blended light in Section 5.2 to obtain constraints on the lens light. Finally in Section 5.4, we illustrate how future high-resolution photometric and spectroscopic observations would clarify the nature of the system.

5.1. Color-Magnitude Diagram

Figure 4 depicts the CMD of stars from the OGLE-III catalog (Szymański et al. 2011) located within a square region with one side length of 240'' centered at the location of KMT-2020-BLG-0414., together with the source position (blue) and the centroid of the red giant clump (red). We measure the centroid of the red giant clump as (VI, I)cl = (2.04 ± 0.01, 15.55 ± 0.02). For the intrinsic centroid of the red giant clump, we adopt (VI, I)cl,0 = (1.06, 14.35) (Bensby et al. 2013; Nataf et al. 2013). This implies that AI = 1.20 and E(VI) = 0.98 toward this direction. For the source color, which is independent of any model, we get (VI)S = 1.82 ± 0.01 by regression of MOA V versus R flux as the source magnification changes and a calibration to the OGLE-III scale using the field-star photometry from the same reductions. Because the source apparent brightness slightly depends on the model, for simplicity, we explicitly derive results for IS = 19.12 and then present a scaling relation for different source magnitudes. From this procedure, we obtain the intrinsic color and brightness of the source as (VI, I)S,0 = (0.84 ± 0.03, 17.92 ± 0.03), suggesting that the source is a mid-G type dwarf (Bessell & Brett 1988). Considering the color/surface-brightness relation of Adams et al. (2018), we obtain

Equation (6)

where the 5% error is given by table 3 of Adams et al. (2018). Then, for any particular model with source magnitude IS, one can infer θ* = 0.943 × 10−0.2(IS – 19.12).

Fig. 4

Fig. 4 CMD for field stars in a 240'' square centered on KMT-2020-BLG-0414. referencing the OGLE-III star catalog (Szymański et al. 2011). The red asterisk, blue dot, magenta dot and green dot represent the positions of the centroid of the red giant clump, the microlens source, the baseline object and the blended light, respectively. The cyan dot marks the position of a naive lens host with M1 = 0.25 M and DL = 0.74 kpc, estimated using the median θE and πE values of the close u0 < 0 solution.

Standard image

5.2. The Blended Light

For KMT-2020-BLG-0414., the baseline object was detected by the OGLE-III survey, (V, I)base = (20.70 ± 0.08, 18.46 ± 0.03). We further consider the statistical errors due to the mottled background from unresolved stars (Park et al. 2004). We follow the approach of Ryu et al. (2020b) utilizing the GalSim package (Rowe et al. 2015) with the readout noise of Udalski et al. (2015). We find σI = 0.08 mag and σV = 0.012 mag, and thus the baseline object has (V, I)base = (20.70 ± 0.14, 18.46 ± 0.09), yielding the blended light of ${(V-I,I)}_{{\rm{B}}}=({3.1}_{-0.6}^{+1.0},19.32\pm 0.20)$. This value is consistent with the lens properties that are predicted by the microlensing light-curve and CMD analyses. For example, using the median θE and πE values of the close u0 < 0 solutions, the host mass M1 = 0.25 M and it would have rough intrinsic brightness and color of MI ∼ 9.8, (V - I)0 ∼ 3.0. Assuming an extinction curve with a scale height of 120 pc, it would have (AI , E(VI))L = (0.38, 0.31) at the lens distance DL = 0.74 kpc. These correspond to (VI, I)L ∼ (3.3, 19.5), which are displayed as the cyan point ("naive lens") in Figure 4 and is quite consistent with the blend.

We also check the astrometric alignment between the source and the baseline object from KMTA imaging. We find that the baseline object lies (0.18'', 0.01'') west and south of the source. Because the source position is derived from difference image analysis on highly magnified images, the uncertainty in the source position (≲ 0.01'') is negligible relative to the error in the baseline position. We estimate the error of baseline position by the fractional astrometric error being equal to the fractional photometric error (Jung et al. 2020), σast = 0.39 σI FWHM = 0.09''. Hence, the baseline object is astrometrically consistent with the source (and thus lens) at the 2σ level. Thus, it is plausible that most or all of the blended light is due to the lens.

The alignment between the source and the baseline object can be immediately checked (i.e., 2021 bulge season) by the Hubble Space Telescope (HST) or by ground-based adaptive optics (AO) mounted on large ground-based telescopes (e.g., Keck, Subaru). Even if the alignment were demonstrated, the blended light could in principle come from a stellar companion to either the source or the lens. However, if the alignment is ≲ 50 mas, an additional stellar companion to the lens would have generated significant deviations on the peak, so the confirmation that the blend is well aligned to the lens could probably rule out the lens-companion scenario. Because the source and the blended light have significantly different colors, the possibility of the source companion can be checked by a measurement of the astrometric offset in different bands (Bennett et al. 2006). It is a priori unlikely that the blended light is primarily due to ambient stars that are unassociated with the event because of the low surface density of stars relative to the 180 mas offset. If high-resolution imaging nevertheless showed that this were the case, it would imply that the parallax was even larger and the lens was less massive and closer than the best-estimated values 7 .

5.3. Bayesian Analysis

In the Bayesian analysis, we choose the log-normal initial mass function of Chabrier (2003) as the mass distribution of the lens. For the bulge and disk stellar number density, we choose the model used by Zhu et al. (2017) and Bennett et al. (2014), respectively. For the dynamical distribution of the disk lens, we assume the disk lenses follow a rotation of 240 km s−1 (Reid et al. 2014) with the velocity dispersion used by Han et al. (2020a). For the source and bulge lens dynamical distributions, we examine a Gaia CMD (Gaia Collaboration et al. 2016, 2018) utilizing the stars within 5' and derive the proper motion of "clump" stars (16.4 < G < 17, 1.9 < Bp Rp < 2.35). We obtain (in the heliocentric frame)

Equation (7)

Equation (8)

We create a sample of 5 × 109 simulated events from the Galactic model. We weight each simulated event, i, by

Equation (9)

where Γi θE,i × μrel,i is the microlensing event rate, and ${ {\mathcal L} }_{i}({t}_{{\rm{E}}})$, ${ {\mathcal L} }_{i}({\theta }_{{\rm{E}}})$ and ${ {\mathcal L} }_{i}({\pi }_{{\rm{E}},{\rm{N}}},{\pi }_{{\rm{E}},{\rm{E}}})$ are the likelihoods of its inferred parameters given the distributions of these quantities. In addition, we adopt the 3σ upper limit of the blended light, IB, limit = 18.9, as the upper limit of the lens flux. We then adopt the mass-luminosity relation of Wang et al. (2018),

Equation (10)

where MI is the absolute magnitude in the I band, and reject trial events for which the lens properties obey

Equation (11)

where AI, DL is the extinction at DL, which is derived by an extinction curve with a scale height of 120 pc.

In Table 5, we list the angular Einstein radius, θE, the microlens parallax, πE, the relative proper motion, μrel, the estimated masses of the individual lens components, M1, M2 and M3, the distance to the lens, DL, and the projected separations to the host, a⊥,2 and a⊥,3, for all of the four 3L1S solutions from the Bayesian analysis. For both solutions, it is found that the host is probably an M1 ∼ 0.3 M M-type dwarf, the second body is an Earth-mass terrestrial planet at a projected separation of a⊥,2 ∼ 1.5 au, and the third body is an object at the planet/brown-dwarf boundary at a projected separation of a⊥,3 ∼ 0.15 au for the close solutions and a⊥,3 ∼ 15 au for the wide solutions. The lens system is located in the Galactic disk with a distance of DL ∼ 1.0 kpc.

Table 5. Physical Parameters

SolutionsClose u0 > 0Close u0 < 0Wide u0 > 0Wide u0 < 0
θE (mas) ${1.475}_{-0.091}^{+0.087}$ ${1.586}_{-0.074}^{+0.074}$ ${1.489}_{-0.083}^{+0.077}$ ${1.574}_{-0.060}^{+0.057}$
πE ${0.470}_{-0.096}^{+0.106}$ ${0.715}_{-0.105}^{+0.096}$ ${0.513}_{-0.097}^{+0.114}$ ${0.840}_{-0.142}^{+0.158}$
M1 (M) ${0.364}_{-0.057}^{+0.072}$ ${0.259}_{-0.034}^{+0.041}$ ${0.340}_{-0.053}^{+0.063}$ ${0.217}_{-0.037}^{+0.045}$
M2 (M) ${1.21}_{-0.22}^{+0.28}$ ${0.96}_{-0.13}^{+0.15}$ ${1.28}_{-0.21}^{+0.25}$ ${0.86}_{-0.13}^{+0.19}$
M3 (MJ ) ${23.3}_{-3.9}^{+4.7}$ ${15.4}_{-2.5}^{+3.3}$ ${16.9}_{-3.0}^{+3.4}$ ${12.5}_{-2.1}^{+2.6}$
DL (kpc) ${1.22}_{-0.23}^{+0.32}$ ${0.80}_{-0.10}^{+0.12}$ ${1.12}_{-0.20}^{+0.27}$ ${0.69}_{-0.11}^{+0.13}$
a⊥, 2 (au) ${1.79}_{-0.28}^{+0.36}$ ${1.26}_{-0.14}^{+0.19}$ ${1.62}_{-0.26}^{+0.30}$ ${1.04}_{-0.16}^{+0.19}$
a⊥, 3 (au) ${0.16}_{-0.03}^{+0.03}$ ${0.12}_{-0.02}^{+0.02}$ ${16.6}_{-2.7}^{+3.2}$ ${11.4}_{-1.8}^{+2.1}$
μhel, N (mas yr−1) ${4.92}_{-0.81}^{+0.51}$ $-{2.82}_{-0.82}^{+0.94}$ ${5.22}_{-0.76}^{+0.49}$ $-{3.58}_{-0.94}^{+1.41}$
μhel, E (mas yr−1) ${6.12}_{-1.92}^{+1.76}$ ${12.07}_{-1.21}^{+1.38}$ ${6.91}_{-1.72}^{+1.58}$ ${13.13}_{-1.30}^{+1.67}$

5.4. Characterizing the Lens System by Future Observations

The highly degenerate 3L1S solutions and their very different π E, with large uncertainties, indicate that the characteristics of the lens system cannot be completely determined by our work. The ambiguous elements mainly include two aspects: the mass and distance of the lens system and the projected separation of the third body. They can be clarified by future high-resolution photometric and spectroscopic observations.

For the lens mass and distance, they can be unambiguously determined by conducting high-resolution AO imaging observations when the source and lens are resolved. Bhattacharya et al. (2018) resolved the source and lens of OGLE-2012-BLG-0950 employing Keck AO and the HST when they were separated by ∼ 34 mas, in a case for which the source and lens had approximately equal brightness. In the present case, the blended light and source also have approximately equal brightness, so the lens and source can be resolved in 2024 provided that the lens contributes a significant part of the blended light. The lens-source resolution can yield the measurement of the lens flux and the lens-source relative proper motion vector, μrel (e.g., Alcock et al. 2001; Kozłowski et al. 2007; Batista et al. 2015). The lens flux would provide an independent mass-distance relationship, and μ rel would further constrain θE (Eq. (1)) and πE (Eq. (2)) by its magnitude and direction, respectively. Together, these can significantly reduce the uncertainties of the physical lens parameters.

For the orbit of the third body, future spectroscopy observations to measure the radial velocity (RV) can determine whether the third body lies inside or outside the planetary orbit. Following the procedure of Han et al. (2019b), we estimate that the close solution has an RV amplitude vsin(i) of order 1 km s−1 with a period of order 0.15 yr, and the wide solution has a vsin(i) of order 100 m s−1 with a period of order 100 yr. These RV amplitudes and differences are big enough to be distinguished by high-resolution spectrometers on VLT/Espresso or future 30 m telescopes. Note that if the lens indeed has comparable brightness to the source, then these observations can be made immediately, i.e., long before the lens and source separate on the sky, because the lens and source RVs likely differ by tens or hundreds of km s−1.

6. Discussion

6.1. Inconsistency of the 2L1S Model

In Section 3, we adopted the perspective that there are no data over peak, and we, in particular, asked how the event would have been analyzed and reported in the absence of such data. Of course, one obvious difference is that the data fit well with the 2L1S model and so there would have been no report of a "third body", but here we see that there would also have been a report of a "major puzzle" about this parallax inconsistency. The derived parallax values in Table 3 (πE = 0.229 ± 0.042 for the u0 > 0 solution or πE = 0.173 ± 0.040 for the u0 < 0 solution) are strongly inconsistent with Equation (3), which was derived from a combination of the well-measured value of θE and the photometric constraints on blended light. Most likely, this would have been "explained" as due to "probable low-level systematics in the KMTA and/or MOA data". Perhaps there would have been some additional commentary about the possibility that the host was a white dwarf, which would enable evasion of the photometric constraints. Then, it is very likely that the final reported parameters would have been given as the static solution, while the physical parameters would have been derived from a Bayesian analysis that simply ignored the parallax measurement. Finally, it would have been pointed out that the apparent discrepancies could ultimately be resolved by future high-resolution follow-up observations.

While the scenarios laid out in the previous paragraph are necessarily somewhat speculative, we believe that the great majority of people familiar with the microlensing-planet literature would broadly agree with this assessment of what would have happened. We recall them here in detail because all of the "explanations", "caveats", etc., in the previous paragraph are completely wrong. In fact, once the peak data are added back into the light curve and a third body is included in the modeling, the supposed "tension" surrounding Equation (3) entirely disappears. We note that the problem of the impact of undetected "third bodies" on microlensing solutions was analyzed by Zhu et al. (2014a). While that study focused on the impact on the measured parameters of the detected planet, the present work shows that higher-order parameters can be affected as well.

6.2. Two Paths for Very Low Mass-Ratio Planets

Over the past two years, the previously empty "tip" of the (log s,log q) diagram has been gradually populated by new discoveries. While KMT-2019-BLG-0842Lb lies just below the "pile up" associated with the Jung et al. (2019) "break" (see Fig. 5), three other recent discoveries (KMT-2018-BLG-0029Lb, OGLE-2019-BLG-0960Lb, KMT-2020-BLG-0414Lb), with q ∼ (6.0, 4.5, 3.6) q, all lie well below it. All four of these recent discoveries were detected via resonant caustics. Moreover, for three of these (all except KMT-2018-BLG-0029Lb), the source trajectory angle with respect to the binary axis was oblique. For two of the four (OGLE-2019-BLG-0960Lb and KMT-2020-BLG-0414Lb), followup observations played a major or dominant role in the detection and characterization.

Fig. 5

Fig. 5 Microlensing parameters (log s,log q) for planetary events (Left: all of the planets; Right: a close-up of q < 10−3 planet), adapted from fig. 11 of Yee et al. (2021), but with the addition of KMT-2020-BLG-0414Lb (red asterisk, average of the median values of the four 3L1S solutions with parallax + planet orbital motion effects). The power-law "breaks" proposed by Suzuki et al. (2016) and Jung et al. (2019) are indicated with the blue lines. Subsequently, there were three planetary events from 2018–2020 that lie well below the cluster of planets near the Jung et al. (2019) "break" (KMT-2018-BLG-0029Lb, OGLE-2019-BLG-0960Lb and KMT-2020-BLG-0414Lb), which are marked with text in the right panel. Together, these three recent discoveries "fill out" the previously empty region at the bottom of the triangular distribution. Solutions are considered to be "unique" (black points) if there are no competing solutions within Δχ2 < 10. Otherwise, they are shown by pairs of green open circles linked by a line segment. However, eight such pairs for which q differs by more than a factor of two are excluded on the grounds that q is not accurately measured. In the right panel, the two magenta dashed lines represent the boundaries between resonant and non-resonant caustics using eq. (59) of Dominik (1999).

Standard image

Due to inhomogeneous (and difficult to model) selection, it is probably not possible to draw precise statistical conclusions from this particular sample. However, the broad features listed above tend to support the idea that there is not a strong break below Neptune mass ratios, as had been previously conjectured. Rather, the conditions and lens geometries required for such detections are rare, including resonant caustic geometries and dense coverage over/near the peak of high-magnification events, often aided by oblique trajectories. In two cases, the dense coverage was provided by KMTNet high (Γ = 1 hr−1), or very high (Γ = 4 hr−1) 3-continent monitoring, and in the other two cases by dense 3-continent follow-up observations.

These characteristics suggest two paths forward for probing the very low-q cold-planet population. First, as discussed by Yee et al. (2021), it should be possible to construct a rigorous statistical sample by systematic investigation of all KMTNet high-magnification events, where the threshold for "high-magnification" would be set at some definite value, like Amax > 20. Each event with pipeline parameters near or above this boundary would require tender-loving care (TLC) reductions to determine if it were truly in the sample, and, if so, it would be subjected to a dense grid search for planets. Both KMT-2018-BLG-0029Lb and KMT-2019-BLG-0842Lb would definitely be recovered by such a search, and it is possible that OGLE-2019-BLG-0960Lb would be recovered as well. These reductions are costly in human effort, but if restricted to high-magnification events, the project would be feasible.

Second, KMT-2020-BLG-0414Lb indicates that follow-up observations of high-magnification events in low-cadence fields can detect the most extreme systems. It is challenging, but not impossible, to derive rigorous statistical conclusions from such a sample. For example, Gould et al. (2010) demonstrated that their sample of 13 very high-magnification (Amax > 200) events was statistically well-grounded because they showed that the μFUN follow-up campaign randomly sampled half of the underlying OGLE-III Amax > 200 events during 2004–2008. This achievement required prodigious human effort because, in the majority of cases, it was not possible to determine which events would be very high magnification based on (often sparse) OGLE-III data alone. Hence, it was necessary to "patrol" a much larger set of OGLE events with 1.3 m SMARTS telescope observations to even determine which events should be densely monitored. Even choosing the events to be patrolled required several hours of human effort per day. This level of effort, for 1–2 planets per year, was the main reason for abandoning this approach once massive surveys were underway.

However, with the advent of KMTNet's 3-continent survey, together with (beginning in full in 2019) its real-time Alert-Finder system (Kim et al. 2018), it has become possible to identify rising high-magnification events with little or no "patrolling". The LCOGT has eight 1 m robotic telescopes at the same sites as KMTNet and a reaction time of about 15 minutes, which allows the rapid necessary coverage for high-magnification events. μFUN is mainly composed of amateur volunteers and has different sites 8 from the current surveys, which can provide targeted coverage for high-magnification events when the survey sites have poor weather. Indeed, our 2020 follow-up program was meant to be a pilot for such a patrol-free (or patrol-lite) high-magnification (A ≳ 20) planet search. This original idea was undermined by COVID-19, which resulted in the closure of two out of three KMTNet observatories for the bulk of the 2020 season. Substantial patrolling was therefore required in this season. For KMT-2020-BLG-0414Lb, the beginning of follow-up observations at "Anow > 10" was actually the result of such patrolling. Nevertheless, the detection of KMT-2020-BLG-0414Lb affirms that this approach is viable.

6.3. Planet Sensitivities of q ∼ 10−5 Planets

For KMT-2020-BLG-0414., thanks to its oblique source trajectory and resonant caustic, the signal of the q ∼ 10−5 planet lasted for about five days (9038 < HJD' < 9043) and ${\chi }_{1{\rm{L}}1{\rm{S}}}^{2}-{\chi }_{2{\rm{L}}1{\rm{S}}}^{2}\gt {10}^{4}$ (without the MOA data on the peak). Two other very low-q planets, KMT-2019-BLG-0842Lb and OGLE-2019-BLG-0960Lb, also have oblique source trajectories and resonant caustics. Thus, it is of considerable interest to compute the planet sensitivities of KMT-2020-BLG-0414. with different source trajectories (α) and caustic structures (s) and to quantitatively determine the contributions of the oblique source trajectory and resonant caustic in the detections of q ∼ 10−5 planets. In addition, Yee et al. (2009) studied the planet sensitivities of the extreme high-magnification microlensing event OGLE-2008-BLG-279, which has similar 1L1S parameters (u0 ∼ 0.0007, τE ∼ 100, ρ ∼ 0.0007) to KMT-2020-BLG-0414.. Because the two events have different followup data coverages (see below), comparing the planet sensitivity of the two events can help provide guidance for the followup strategy of very low-q planets.

We apply the method of Rhie et al. (2000) to evaluate the planet sensitivities, which was also followed by Yee et al. (2009). In brief, we first simulate 2L1S curves from a grid of (α, s), using (t0, u0, τE, ρ, q, IS, IB) of the best-fit 3L1S model with parallax and planet orbital motion. The epochs and the corresponding residuals of the mock 2L1S curves are the same as the real observed data. The grid consists of 360 values equally spaced between 0° ≤ α ≤ 359° and 151 values equally spaced between 0.5 ≤ s ≤ 2.0. Yee et al. (2009) generated 2L1S curves for q = 10−3, 10−4, 10−5, 10−6. Here we only study q = 1.08 × 10−5, because in the present context, we are only interested in the sensitivity to q ∼ 10−5 planets. We then fit the mock 2L1S curves using the 1L1S model allowing (t0, u0, τE, ρ) to vary and compute the Δχ2 relative to the curve without any planet.

The resulting Δχ2 as a function of (s cosα, s sinα), depicted in Figure 6, has three important features compared to the lower-left panel of figure 6 of Yee et al. (2009). First, for both cases, the resonant caustics have the highest sensitivities to a q ∼ 10−5 planet, while the observed data are sensitive to a q ∼ 10−5 planet over a wide range, with |log s| ≲ 0.14 applying a detection threshold of $\Delta {\chi }_{{\rm{\min }}}^{2}\sim 100$. Second, KMT-2020-BLG-0414. is only sensitive to q ∼ 10−5 planets from oblique source trajectories (|sinα| ≲ 0.5), while OGLE-2008-BLG-279 is quite sensitive for all source trajectories. The planetary signals of perpendicular and nearly-perpendicular source trajectories mainly occur on the peak, so the different α distributions are due to the different data coverage on the very high-magnification region. OGLE-2008-BLG-279 has nearly continual coverage during A ≥ 100, while KMT-2020-BLG-0414. has no coverage during ∼ 40% of the A ≥ 100 light curve, and its peak was only observed by MOA with a cadence of Γ ∼ 4 hr−1. Third, for oblique source trajectories, KMT-2020-BLG-0414. has a much higher sensitivity, with several hundred times higher Δχ2 for some resonant caustics. The planetary signals of resonant caustics together with oblique source trajectories are mainly detectable at intermediate magnification. OGLE-2008-BLG-279 has only very sparse coverage on A < 100, while KMT-2020-BLG-0414. was observed several hundred times more during 20 < A < 100. These features are qualitatively similar to those obtained in Dong et al. (2006), where they compared the sensitivity of q = 10−5 planets from actual data for the extremely high-magnification microlensing event OGLE-2004-BLG-343 with incomplete coverage over peak (see their fig. 6) with those from simulated data with complete coverage (see their fig. 8) using the method of Rhie et al. (2000).

Fig. 6

Fig. 6 Planet sensitivity as a function of (s cosα, s sinα) for the observed data of KMT-2020-BLG-0414., with q = 1.08 × 10−5. Δχ2 represents the χ2 difference between the mock 2L1S curves fitted by the 1L1S model and the curve without any planet. The black solid line corresponds to the Einstein ring (s = 1), and the two black dashed lines signify the boundaries between resonant and non-resonant caustics. Different colors indicate different Δχ2.

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The planet sensitivity studies of KMT-2020-BLG-0414. and OGLE-2008-BLG-279 provide two important implications for followup observations. First, for the very high-magnification region (A ≳ 100), dense or even continual observations are of critical importance. Second, the followup observations should begin at intermediate magnification (e.g., the current threshold of the LCOGT & μFUN followup program is A = 20), in order to capture the signals of oblique source trajectories. Assuming at least four data points are required to characterize the planetary caustic crossing, the minimum required cadence at intermediate magnification is

Equation (12)

where t* = ρτE = θ*/μrel is "source-crossing timescale", and one can adopt a relatively conservative lower limit on t* by adopting μrel = 10 mas yr−1 and estimate θ* by the rough source position on the CMD. On the declining part of the light curve, Γmin can be most accurately estimated because Amax is well known unless the rising side has almost no coverage due to weather. On the rising side, Γmin is still more uncertain because Amax is generally not known well before the peak. Nevertheless, for events that eventually reach very high magnification, it is often possible to reliably predict that

Equation (13)

where n ∼ 3 is a typical value. In addition, this cadence should be reached by followup alone, without a combination of survey cadence. First, independent observations of followup and survey can doubly confirm the planetary signal. Second, part of the observing window on the planetary perturbation could be lost due to weather. Third, if an anomaly has occurred or the quality of the real-time survey photometry is not good enough, Γmin could be underestimated.

6.4. Multiple Low Mass-Ratio Companions

Including KMT-2020-BLG-0414., 15 triple-lens events have been published. Among these, six lens systems contain two planets orbiting a star and seven consist of a planet in a binary-star system (for details, see table 1 of Han et al. 2021). OGLE-2016-BLG-0613L (Han et al. 2017) and KMT-2020-BLG-0414L are composed of a star, a low-mass brown dwarf and a planet 9 . Among the eight systems containing a host and two low mass-ratio (q < 0.1) companions, five were detected by a high-magnification event: OGLE-2006-BLG-109 (u0 = 0.0035, Gaudi et al. 2008; Bennett et al. 2010), OGLE-2012-BLG-0026 (u0 = 0.0088, Han et al. 2013; Beaulieu et al. 2016; Madsen & Zhu 2019), OGLE-2018-BLG-0532 (u0 = 0.0079, Ryu et al. 2020b), KMT-2019-BLG-1953 (u0 = 0.0007, Han et al. 2020b) and KMT-2020-BLG-0414. (u0 = 0.0007) 10 . High-magnification events provide an efficient channel for multiple low mass-ratio companions because the source trajectory goes very close to the host, where each planet/BD induces distortions in the magnification profile via their central or resonant caustics (Gaudi et al. 1998).

There have been only two microlensing studies about the occurrence rate of systems with multiple low mass-ratio companions. Using the one two-planet system OGLE-2006-BLG-109L among the 13 μFUN A > 200 sample, Gould et al. (2010) found that the frequency of solar-like systems is 1/6 for all planetary systems. Utilizing the two multiplanetary systems OGLE-2006-BLG-109L and OGLE-2014-BLG-1722L, and the detection efficiency of the six-year MOA survey combined with the four-year μFUN follow-up observations, Suzuki et al. (2018) estimated that 6% ± 2% of stars host two cold giant planets. The detection of KMT-2020-BLG-0414L suggests that the new follow-up program for high-magnification events can also give an estimate of the occurrence rate of systems with multiple low mass-ratio companions.

In addition, although the new follow-up program aims to observe events located in KMTNet Γ ≤ 1 hr−1 fields, it is still important to follow up very high-magnification events located in KMTNet Γ = 4 hr−1 fields. First, a simulation of Zhu et al. (2014b) indicates that even KMTNet Γ = 6 hr−1 cadence is not intensive enough to capture the subtle anomalies for very high-magnification events. This has been demonstrated by the two less secure multiplanetary events OGLE-2018-BLG-0532 and KMT-2019-BLG-1953, for which a cadence of Γ = 4 hr−1 was only barely adequate to detect the second planet. Second, the survey observations could suffer from nonlinearity or saturation on the very bright peak of very high-magnification events. For KMT-2020-BLG-0414., its I = 11.1 peak is too bright for the current surveys with their normal exposure time (60 s for KMTNet with three 1.6 m telescopes, 100-120 s for OGLE with a 1.3 m telescope and 60 s for MOA with a 1.8 m telescope). The LCOGT and most of the μFUN telescopes have smaller apertures and more flexible exposure time, so the new follow-up program can provide supplementary coverage for the very bright peak of very high-magnification events in KMTNet Γ = 4 hr−1 fields.

Acknowledgements

W.Z. thanks Subo Dong for fruitful discussions. We thank the anonymous referee for an especially valuable report that helped greatly. W.Z., S.M. and X.Z. acknowledge support by the National Natural Science Foundation of China (Grant Nos. 11821303 and 11761131004). Work by C.H. was supported by grants from the National Research Foundation of Korea (2019R1A2C2085965 and 2020R1A4A2002885). Work by JCY was supported by JPL grant 1571564. This research has made use of the KMTNet system operated by the Korea Astronomy and Space Science Institute (KASI) and the data were obtained at three host sites of CTIO in Chile, SAAO in South Africa and SSO in Australia. This research uses data obtained through the Telescope Access Program (TAP), which has been funded by the TAP member institutes. The MOA project is supported by JSPS KAK-ENHI (Grant Nos. JSPS24253004, JSPS26247023, JSPS23340064, JSPS15H00781, JP16H06287, JP17H02871 and JP19KK0082). This research is supported by Tsinghua University Initiative Scientific Research Program (Program ID 2019Z07L02017). Wei Zhu was supported by the Natural Sciences and Engineering Research Council of Canada (NSERC) under the funding (reference #CITA 490888-16).

Appendix A: The difference in s2

For the 3L1S model, in fact, what the light curve is sensitive to is not directly s2, i.e., the angular separation between M2 and M1, scaled to θE. Rather, it is directly sensitive to "x2", which is the offset between M2 and the center of mass of the body(ies) interior to s2, scaled to θE, interior, i.e., the Einstein radius associated with the mass interior to s2. Hence, we do not expect the s2 from the various solutions (in particular, the wide and close topologies) to be equal, but rather their associated x2.

For example, for the wide 3L1S static solution, M1 is the only body interior to s2. Hence, its position is also the center of mass. However, ${\theta }_{{\rm{E}},{\rm{interior}}}=\,{\theta }_{{\rm{E}}}/\sqrt{1+{q}_{3}}$. Hence,

Equation (A1)

For the corresponding close solution, θE, interior = θE. However, the center of mass of the material interior to s2 is offset from M1 by Δ x = s3 q3/(1 + q3) and thus

Equation (A2)

That is, as expected, x2, close = x2, wide to within 2.8 × 10−4.

Footnotes

  • In fact, Yee et al. (2021) reported that "semi-resonant" caustics, which have not quite merged but still have long magnification ridges extending from the central caustic, as well as exceptionally large planetary caustics, are just as sensitive as resonant caustics.

  • Although OGLE-2017-BLG-0173 has a best-fit solution of q ∼ 8 q, its two degenerate solutions have q ∼ 21 q at Δχ2 = 3.5 (Hwang et al. 2018).

  • In fact, this V-band to I-band ratio applies only to the "normal cycle" of KMT observations. During the latter part of the season (including the peak of KMT-2020-BLG-0414), these normal-cycle observations were supplemented by an end-of-night sequence of eastern fields, which was purely in the I-band. For the low-cadence field BLG32, these end-of-night observations accounted for ∼ 30% of the total near the peak of the event.

  • The LCOGT & μFUN Follow-up Team recognized the KMTA photometric centroid shift by its noisy curve and thus started follow-up observations for security, although Anow did not meet the A ≳ 20 threshold. In fact, the actual magnification at that time was about 35.

  • One exception to this limit would be if the lens were a massive remnant.

  • Or the host could conceivably be a white dwarf.

  • For OGLE-2016-BLG-0613L, there are two degenerate solutions (a planet + binary stars) disfavored by $\Delta {\chi }^{2}\ge 10$.

  • 10 

    Here we adopt the mean u0 of the underlying 1L1S event for degenerate solutions.

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