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The Influence of Planet Nine on the Orbits of Distant TNOs: The Case for a Low-perihelion Planet

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Published 2018 September 14 © 2018. The American Astronomical Society. All rights reserved.
, , Citation Jessica Cáceres and Rodney Gomes 2018 AJ 156 157 DOI 10.3847/1538-3881/aad77a

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Abstract

The hypothesis of an additional planet in the outer solar system has gained new support as a result of the confinement noted in the angular orbital elements of distant trans-Neptunian objects. Orbital parameters proposed for the external perturber suggest semimajor axes between 500 and 1000 au, perihelion distances between 200 and 400 au for masses between 10 and 20 M. In this paper, we study the possibility that lower perihelion distances for the additional planet can lead to angular confinements as observed in the population of objects with semimajor axes greater than 250 au and perihelion distances higher than 40 au. We performed numerical integrations of a set of particles subjected to the influence of the Sun, the known giant planets, and the putative perturber during the age of the solar system and compared our outputs with the observed population through a statistical analysis. Our investigations showed that lower perihelion distances from the outer planet usually lead to more substantial confinements than higher ones, while retaining the Classical Kuiper Belt as well as the ratio of the number of detached with perihelion distances higher than 42 au to scattering objects in the range of semimajor axes from 100 to 200 au.

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1. Introduction

The existence of trans-Neptunian objects (TNOs) with high-perihelion distance (q ≳ 40 au) and semimajor axis (a ≳ 200 au) cannot be explained by the sole influence of the known planets. Thus, several mechanisms have been proposed to explain the existence of these objects, whose best known member is Sedna (a = 482 au and q = 76 au; Brown et al. 2004). Some of these mechanisms are: the interaction of the Sun with other stars when it was still in its birth cluster and stellar flybys were common (Brasser et al. 2012; Dukes & Krumholz 2012), the capture of planetesimals from the external disk of another star (Kenyon & Bromley 2004; Morbidelli & Levison 2004), a planet that could have existed temporarily in the scattered disk (Gladman & Chan 2006), or an existing yet undiscovered planet (Gomes et al. 2006).

From a few years ago, several patterns have been noticed in distant TNOs supporting the hypotheses of an outer planet in the solar system. After announcing the discovery of an object with perihelion distance similar to that of Sedna, 2012 VP113 (a = 256 au and q = 80 au), Trujillo & Sheppard (2014) noted that objects with a > 150 au and q > 30 au exhibit a confinement in their argument of perihelion (ω). They argued that under the influence of the known planets, the argument of perihelion of these objects would circulate in a fairly short and varying timescale. On the other hand, they showed that a super-Earth mass planet in a circular and low-inclination orbit with semimajor axis between 200 and 300 au could lead to long-period ω- libration around 0° for Sedna-like objects, but not for objects with lower perihelia. This opened the interesting possibility that other configurations of an outer planet might give the suitable tuning.

Later, Batygin & Brown (2016a) noted that TNOs with a > 250 au and q > 30 au are confined not only in ω, but also in longitude of the ascending node (Ω). They showed that the presence of a distant, eccentric, and massive planet could reproduce such confinements as well as perihelion detachment of distant TNOs as a consequence of secular and resonant interactions (see also Batygin & Morbidelli 2017 and references therein). This planet (hereafter named Planet 9, whose orbital parameters will be denoted with the subscript 9) would roughly share the same orbital plane as those of the confined objects and would be apsidally anti-aligned with them. Planet 9 would also predict the existence of apsidally aligned and high-perihelion objects, if a wide distribution of perihelion is initially assumed (see also Khain et al. 2018), and objects that would be compatible with the Centaurs of high semimajor axis and high inclination. Likewise, it offers an explanation for the origin of highly inclined TNOs (i > 60°) with a < 100 au (Batygin & Brown 2016b) and the high inclination of the recently discovered long-period TNO, 2015 BP519 (q = 36 au; Batygin & Morbidelli 2017; Becker et al. 2018).

Brown & Batygin (2016) showed that confined TNOs orbits can be produced by Planet 9 with the following orbital parameters1 : 200 au < q9 < 400 au, 500 au < a9 < 1000 au, i9 ∼ 30°, and mass 10 M < m9 < 20 M. By comparing the allowed orbital paths and estimated brightness of the planet to previous and ongoing surveys, they indicate that Planet 9 would be near aphelion with an apparent visual magnitude between 22 and 25.

Subsequent works focused on restricting the location of Planet 9 on its orbit from the reduction of the residuals in Saturn's orbital motion based on Cassini data (Fienga et al. 2016; Holman & Payne 2016a), or in Pluto's orbit (Holman & Payne 2016b), or assuming that several of the distant TNOs are in mean motion resonance (MMR) with the planet (Malhotra et al. 2016; Millholland & Laughlin 2017).

An outer planet also provides a better explanation for the fact of there being an excess of bright large semimajor axis Centaurs with respect to classical ones than a scenario without an additional planet (Gomes et al. 2015). Moreover, Gomes et al. (2017; see also Bailey et al. 2016 and Lai 2016) provide an explanation for the current inclination of the planetary system invariable plane with respect to the Sun's equator of ∼6°. They arrived at parameters for the distant planet compatible with those found by Brown & Batygin (2016) although with possible larger eccentricities corresponding to a given semimajor axis.

As for the proposed mechanisms for its origin, Planet 9 could have been originally dispersed from the giant planets region. In order to avoid that repeated close encounters with a giant planet could end in the ejection of the scattered planet, the perihelion distance of its orbit would have to be lifted by some mechanism. These might include its gravitational interaction with the Sun's birth cluster (Brasser et al. 2006, 2012) or dynamical friction with a planetesimals disk located beyond 100 au (Eriksson et al. 2018) or with an either massive and short-lived or low-mass and long-lived gas disk (Bromley & Kenyon 2016). Other proposed scenarios suggest the capture of a planet from another star system or the capture of a free-floating planet in the solar birth cluster (Li & Adams 2016; Mustill et al. 2016; see, however, Parker et al. 2017).

Brown & Batygin (2016) present tables with probabilities for a Planet 9 with a given semimajor axis and eccentricity to induce a favorable orbital confinement of large semimajor axis TNOs. One of their criteria to choose the best orbit for Planet 9 is to rule out those that produce too many high-perihelion and low-semimajor axis TNOs. Here we analyze the evidence of a distant planet, without neglecting the case of planets with low perihelion that were naturally neglected in Brown & Batygin (2016), since they would assumedly produce an excess of high-perihelion TNOs for relatively small semimajor axes. We particularly analyze these low-perihelion planets' influence on the Kuiper Belt and on the relation between scattered and detached objects. In Section 2, we describe the methods used to test the influence of Planet 9 on large semimajor axis TNOs. We present our results in Section 3. In Section 4, we emphasize the case of low-perihelion planets. In Section 5, we present our conclusions.

2. Methods

The origin of the detached objects (defined as minor bodies with a > 50 au and q > 40 au) with a ≲ 200 au can be explained as a result of the increase of the perihelion distance of scattered disk objects (bodies with a > 50 au and 30 au < q < 40 au) via resonant capture with Neptune associated with the Kozai mechanism. These objects may still be experiencing those resonances or they may have been released from the resonant coupling MMR-Kozai during the migration of Neptune after the instability phase of the solar system (Gomes et al. 2005a; Morbidelli et al. 2005; Tsiganis et al. 2005), when their orbital eccentricities were low enough (Gomes et al. 2005b; Gomes 2011; Brasil et al. 2014).

Our analysis is motivated by the TNOs with q ≥ 40 au and a ≥ 250 au, whose existence cannot be explained by the current orbital configuration of the giant planets. Currently, there are nine2 objects within this category observed in more than one opposition in the Minor Planet Center (MPC) database.3 As shown in Figure 1 they have Ω < 220°, a confinement of 131fdg7 in ω (between ω = 293fdg6 and ω = 65fdg3), and two likely confinements in longitude of perihelion (ϖ), where the main confinement, of 102fdg6, is composed of seven objects and located around ϖ = 60fdg5, and the secondary one, represented by the two remaining objects, around ϖ = 254fdg6. These objects have q < 81 au and i < 26°. We decided to neglect objects with smaller semimajor axis and perihelion distance than those above mentioned unlike other works (e.g., Batygin & Brown 2016a) concerning Planet 9 since the largest a and q are, the likeliest are that these objects have not experienced an important close encounter with Neptune in a fairly recent past. Thus these objects are prone to keep the angular alignment induced by Planet 9. We note that considering distant TNOs with these higher lower boundaries in semimajor axis and perihelion distance, and also the existence of a secondary clustering, the angular confinement is more remarkable for ϖ and ω than for Ω. Surveys carried out near the ecliptic plane would favor the detection of objects with ω = 0° or ω = 180°. The fact that there is no confinement around ω = 180° and that several of these objects were discovered in off-ecliptic surveys argue that the confinement around ω = 0° is not an effect due to observational bias (Trujillo & Sheppard 2014). It should be noted, however, that even though the clustering in ω observed near 0° is not an artifact of observational bias, a real clustering of ω near 0° will be observationally intensified due to the bias above mentioned.

Figure 1.

Figure 1. Longitude of the ascending node, argument of perihelion and longitude of perihelion as a function of the semimajor axis for all trans-Neptunian objects observed in more than one opposition and up to a = 1000 au, those with a ≥ 250 au and q ≥ 40 au are highlighted in red.

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We performed numerical integrations for the age of the solar system considering different combinations of perihelion distance, inclination and argument of perihelion for two semimajor axes of Planet 9, a9 = 700 au and a9 = 1500 au, where for the models with the small semimajor axis we consider a mass of $3\times {10}^{-5}\,{M}_{\odot }$, and a mass of $5\times {10}^{-5}\,{M}_{\odot }$ for the other case. The tested grids are shown in the first column of Table 1. The nomenclature for each model means a9i9ω9q9m9, where the semimajor axis and perihelion distance are in au, the inclination and argument of perihelion in degree, and the mass in ${10}^{-5}\,{M}_{\odot }$ (∼3.3 M).

Table 1.  Mean and Standard Deviation (STD) of the Angular Distance between the Particles' Primary Center of Clustering and the Same Angle for Planet 9, Computed for the Last 500 Myr

Model ΔΩ (deg) Δω (deg) Δϖ (deg)
  Mean Std Mean Std Mean Std
a1500-10-0-100-5 107.0 7.0 73.9 21.7 180.2 18.7
a1500-30-0-60-5 78.4 18.5 181.8 17.7 248.9 4.4
a1500-30-0-100-5 127.4 15.8 252.5 13.2 232.2 2.4
a1500-30-0-200-5 307.0 93.5 265.6 75.8 174.6 19.3
a1500-30-0-300-5 351.2 55.1 185.1 28.2 172.4 10.8
a1500-30-90-60-5 211.4 75.7 216.2 82.5 184.8 85.4
a1500-60-0-100-5 265.5 12.8 305.6 17.9 201.8 5.4
a700-10-0-100-3 193.5 68.4 58.7 98.8 233.8 9.2
a700-30-0-60-3 112.9 77.5 182.5 71.0 182.1 62.0
a700-30-0-100-3 125.9 71.0 255.6 66.5 191.4 13.8
a700-30-0-200-3 316.0 7.1 266.7 7.0 223.1 4.1
a700-30-0-300-3 148.5 100.1 227.2 81.2 239.6 27.1
a700-30-90-60-3 244.3 68.9 333.5 84.3 229.1 19.6
a700-60-0-100-3 100.9 82.2 142.1 75.3 198.1 21.5

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The initial conditions are given in relation to the plane perpendicular to the resultant angular momentum vector of the four known giant planets (hereinafter referred to as iv4) in their current configuration, which defines the initial orbital elements for the known giant planets. Besides these, the system is made up also of an external perturber and 10000 test particles4 with orbital elements similar to those that would be expected some time after the instability phase of the giant planets under the Nice Model (Gomes et al. 2005a; Morbidelli et al. 2005; Tsiganis et al. 2005): 200 au < a < 1000 au, 30 au < q < 40 au, 0° < i < 10° and the remaining orbital elements uniformly distributed. The lower limit for the particles' semimajor axes stands for the fact that we are only interested in large semimajor axis TNOs to better characterize their confinement. Due to the torque exerted by the ninth planet in an inclined orbit on known planets the initial reference plane will precess with respect to the invariable plane of the system, so that our outputs are converted relative to the instantaneous iv4 plane.

The integrations were done with the MERCURY package hybrid integrator (Chambers 1999). To profit from a multi-core supercomputer, for each model we first ran an integration with just the planets, saving their coordinates at each 10 years for later use. After that we performed 100 numerical integrations, each in a different core, reading the coordinates from a file produced by the run with just the planets. These integrations with particles were done normally with the same timestep of 0.5 year, but at every 10 years, we corrected back the planets coordinates to those produced by the original integration with no particles. This is quite an easy and reliable procedure. The deviation of the planets after 10 years (20 timesteps) is always quite small since the particles are massless and the difference between the integration with particles and the original one with just the planets comes solely from the fact that the (hybrid) integrator can enter into the classic integration mode (Bulirsch-Stoer) at close encounters of particles with planets. We thus modified the code for the hybrid integrator to implement this procedure. For each time considered in the analyses, and for each particle, we associate that time and ten other neighboring ones, five subsequent ones and five previous ones, entailing a total Δt = 106 year, in order to improve the statistics. In 106 years, the circulation of the angles Ω, ω, and ϖ for the distant TNOs and Planet 9 is quite small so that this procedure does not spoil the investigation of confinements.

For the simulated particles belonging to a range in a, q, and i similar to that of the observed objects, our analysis consists of determining the time evolution of (i) the highest and second-highest peaks in Ω, ω, and ϖ as determined by histograms of the distribution of those angles, (ii) the angles corresponding to the middle of the bins that yielded the highest and second-highest peaks, and (iii) the confinements in Ω, ω, and ϖ. These are described in detail below.

The highest and second-highest peaks are determined for each time by performing histograms of the number of particles that have their Ω, ω, and ϖ inside the histograms' bins. These particles are a subset of the simulated particles whose semimajor axes, perihelion distances, and inclinations belong to the interval 250 au ≤ a ≤ 1000 au, 38 au ≤ q ≤ 90 au and 0° ≤ i ≤ 30°. The absolute number of particles in each bin is transformed into frequencies, N, given by the number of particles associated to that bin divided by the total number of particles in all bins. The bins are 30° wide so there is a total of 12 bins. Thus, a flat distribution yields a frequency of 1/12 for each bin. The idea of choosing a bin 30° wide is based on visual inspection of the clustering of some angles during the evolution of the simulated TNOs. We saw that this clustering can be quite narrow and 30° was chosen so as to capture this peculiar feature. For each time we make 30 histograms, which differ from each other in the initial angle, varying from 0° to 29°, so that we can more accurately determine the bin where there is the greatest clustering of angles, which is the one with highest N in all 30 histograms for the same time. Figure 2 depicts the construction of the histograms for Ω, ω, and ϖ for three different initial positions of the bins. In both Ω and ϖ, we see the appearance of two peaks in the angular frequencies. Unless the distribution is totally flat, which is very unlikely, there is always a bin with a highest frequency. The secondary frequency is defined whenever there is a secondary peak in the histogram. It is not the second-highest frequency in the histogram, which would often be associated just to a bin next to the highest frequency. Note that we are thus obtaining the values corresponding to two confinements with a minimum angular distance from each other of 60°. In this way, we obtain the highest (N1) frequency and the respective secondary one (N2) for each time and their respective associated angles.

Figure 2.

Figure 2. Frequencies in Ω, ω, and ϖ for the model a1500-30-0-60-5 at a time t = 2.18 Gyr showing three different beginnings of the first bin at 0°, 12°, and 22° in blue, gray, and red, respectively; out of a total of 30 considered in each time to calculate the highest and secondary frequencies in these orbital elements. For Ω and ϖ, we can distinguish a principal and a secondary confinement, which are distant from one another of ∼180°. There is no secondary frequency in ω.

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The idea behind this analysis is that a bin with a high frequency corresponds to a relevant confinement in the angular interval defined by the bin. The measurement of the secondary frequency is motivated not only from the observational data shown in Figure 1 where the distribution of ϖ suggests the existence of two confinements, but also on visual inspection of the evolution of the angular confinements produced by the simulations.

We also perform a confinement test similar to that in Brown & Batygin (2016). For each time, we also consider the particles that belong to the interval 250 au ≤ a ≤ 1000 au, 38 au ≤ q ≤ 90 au and 0° ≤ i ≤ 30° and we complete 100 iterations, where in each iteration, we randomly select nine objects from the set of particles (because we are considering nine observed distant TNOs); for Ω and ω, we calculate the confinement for the nine objects and for ϖ, we determine the smallest possible confinement for seven of those nine objects (since, as mentioned above, we are assuming that there are two confinements in ϖ). Thereby, we obtain for each time the average and standard deviation of the confinements.

3. Results

The time evolutions of the highest and secondary frequencies in the angles Ω, ω, and ϖ obtained from histograms show better defined angular confinements during the first billion years in almost all our models. Figures 3 and 4 present the results for two extreme cases of perihelion distances, q9 = 60 au and q9 = 300 au, both for semimajor axis of Planet 9 of 1500 au. These figures suggest that higher frequencies, therefore, narrower confinements, are usually associated with smaller perihelion distances of Planet 9. This trend is also true for models with a9 = 700 au.

Figure 3.

Figure 3. First and secondary peaks in the angular frequencies as a function of time shown with blue and red, respectively, for the model a1500-30-0-60-5.

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Figure 4.

Figure 4. Same as Figure 3 for the model a1500-30-0-300-5. The values of the highest and secondary frequencies are quite low, mainly in Ω and ω where both primary and secondary frequencies have similar low values implying that there is no well defined confinement.

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The angles corresponding to the highest and second-highest peaks in the frequencies are calculated in relation to that of Planet 9 (ΔΩ, Δω, and Δϖ). In most of our models, Planet 9 leads to a shepherding in ϖ of the set of more tightly confined particles (those within the angular range corresponding to the highest frequency), and in several of our models, this is also true for the particles belonging to the second confinement. Figure 5 shows an example of this behavior, where the angular distance between both confinements in ϖ is not constant and at 4.5 Gyr it is ∼100°. We also notice that the highest and secondary frequencies switch positions several times. When we compare this with Figure 3, we see that this switching happens when the highest and secondary frequencies have similar values. For Ω and ω, the angular distance between the particles' center of angular clustering and the corresponding angle of Planet 9 is not so well defined in time, but in some of our models, the relative distances ΔΩ and Δω corresponding to the highest frequency also remain constant for about the last Gyr. Models with large perihelion distances show a large dispersion in the relative angles (Figure 6).

Figure 5.

Figure 5. Evolution of the angular elements of the particles' orbits in relation to those of the Planet 9 corresponding to the highest and secondary frequencies shown with blue and red colors respectively, for the model a1500-30-0-60-5. For ϖ, the main and secondary confinements exchange positions several times until ∼2 Gyr, when the main confinement is kept roughly unchanged.

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Figure 6.

Figure 6. Same as Figure 5 for the model a1500-30-0-300-5. The particles do not maintain an approximately constant relative distance for the last billion years in neither ΔΩ nor Δω, as expected for great perihelion distances of Planet 9.

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Table 1 shows the average and standard deviation taken for the last 0.5 Gyr of simulation time, of the angular distance between the center of angular clustering and the corresponding planetary angle. We see that for ϖ, this distance varies inside the range 172fdg4–248fdg9, thus giving a dispersion of 76fdg5. The average of this angular distance is 206fdg6, which suggests the likely position of Planet 9' longitude of perihelion at ∼267°. For Ω and ω, the relative angular distances are not well defined but vary roughly uniformly around all 360° range. This is true even if we just consider the cases of smaller standard deviations where the clustering position is better defined.

Our analysis of confinement as a function of time confirms our previous results. In all models, a better confinement for the particles is reproduced for ϖ than for Ω or ω and planets with smaller perihelion distances are associated with better confinements (compare Figures 7 and 8). For models with q9 ∼ 300 au, the confinements, mainly in Ω and ω, are near to what would be expected in the case of a randomly produced uniform distribution in these angular elements when the procedure indicated in the Section 2 is applied.

Figure 7.

Figure 7. Confinement mean and its standard deviation in Ω, ω, and ϖ as a function of time shown with dark and light brown, respectively, for the model a1500-30-0-60-5.

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Figure 8.

Figure 8. Same as Figure 7 for the model a1500-30-0-300-5. From about 1 Gyr, results are very similar to those that would be expected in the case of a random distribution.

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In Table 2, we depict the maximum and mean values of the collection of highest frequencies (main confinements) in Ω, ω, and ϖ of the particles considering the full integration time (see also Figure 9) and the last 500 Myr, for all our models. The reliability of the numbers presented in Table 2 and plotted in several figures depend on the number of points used to build the statistics for each time. Since particles are continually ejected by the planets during the simulation, the worst cases are always near the end of the integrations. Moreover, planets with lower perihelion distances eject more particles through the whole evolution than those with higher perihelion distances. In most of the cases, and for any time, we always have more than 50 points to build the statistics, anyways. For one specific case, as commented in Section 2, we doubled the number of points. For that case, there were several times with less than 20 points and we assessed that there were not enough points to produce reliable numbers for the end of the simulation (the last 0.5 Gyr). As for the other cases that were not doubled, the worst one is for Planet 9 with a9 = 700 au, i9 = 30°, ω9 = 0°, and q9 = 60 au, for which we have 24 times with less than 50 points, but just two times with less than 20 (17 and 16 points). Also, as a portion of the results shown in Table 2 are given in averages for at least the last 0.5 Gyr, even a small randomization due to small numbers can be averaged out. For planets with the lowest perihelion distances (60 and 100 au), however, one must consider with caution the results described by the maxima.

Figure 9.

Figure 9. Mean values of N1 in Ω, ω, and ϖ (represented by circles, triangles, and squares, respectively) calculated for the complete integration time for models with i9 = 30° and ω9 = 0°. The gray color represents models with a9 = 1500 au and the violet one those with a9 = 700 au.

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Table 2.  Maximum and Mean Values of the Angular Frequencies Corresponding to the Narrowest Confinements Calculated Considering both the 4.5 Gyr and the Last 500 Myr of Integration Time

Model N1 in Ω N1 in ω N1 in ϖ
  4.5 Gyr last 500 Myr 4.5 Gyr last 500 Myr 4.5 Gyr last 500 Myr
  max mean max mean max mean max mean max mean max mean
a1500-10-0-100-5 0.362 0.226 0.219 0.183 0.313 0.202 0.194 0.164 0.472 0.283 0.376 0.319
a1500-30-0-60-5 0.567 0.331 0.515 0.359 0.499 0.299 0.436 0.308 0.714 0.456 0.665 0.483
a1500-30-0-100-5 0.621 0.358 0.304 0.236 0.595 0.346 0.337 0.266 0.749 0.466 0.651 0.545
a1500-30-0-200-5 0.367 0.229 0.196 0.163 0.323 0.207 0.219 0.175 0.464 0.278 0.269 0.241
a1500-30-0-300-5 0.265 0.178 0.175 0.152 0.210 0.150 0.182 0.151 0.395 0.244 0.321 0.266
a1500-30-90-60-5 0.397 0.244 0.354 0.259 0.405 0.251 0.344 0.262 0.493 0.293 0.318 0.248
a1500-60-0-100-5 0.394 0.242 0.332 0.255 0.326 0.209 0.220 0.176 0.425 0.259 0.383 0.348
a700-10-0-100-3 0.848 0.473 0.848 0.530 0.681 0.386 0.494 0.336 0.768 0.486 0.651 0.456
a700-30-0-60-3 0.803 0.447 0.803 0.520 0.688 0.389 0.688 0.439 0.786 0.440 0.786 0.518
a700-30-0-100-3 0.494 0.292 0.276 0.214 0.479 0.285 0.373 0.257 0.603 0.349 0.479 0.372
a700-30-0-200-3 0.470 0.283 0.470 0.324 0.525 0.311 0.458 0.313 0.744 0.459 0.707 0.577
a700-30-0-300-3 0.402 0.253 0.343 0.263 0.409 0.251 0.395 0.283 0.620 0.394 0.443 0.325
a700-30-90-60-3 0.582 0.336 0.582 0.394 0.459 0.275 0.415 0.308 0.603 0.349 0.587 0.410
a700-60-0-100-3 0.832 0.465 0.553 0.372 0.766 0.429 0.653 0.422 0.882 0.534 0.632 0.458

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In general, lower perihelion distances of Planet 9 produce better defined confinements in the distant TNOs. However, a constraint that an outer planet with a low-perihelion distance should satisfy is the preservation of the Classical Kuiper Belt. Another important constraint refers to the right ratio of observed detached to scattering objects, since a distant planet tends to overpopulate the region of the detached objects. These will be the subjects of the next section.

4. Other Tests for Planet 9 with Low-perihelion Distance

In this section, we show the results of the influence of Planet 9 with low-perihelion distance on the relation between the scattered disk and detached populations within the range 100 au < a < 200 au and on the Classical Kuiper Belt Objects (KBOs).

4.1. The Influence of Planet 9 on the Relation between Scattered and Detached Objects

Brown & Batygin (2016) searched for the best Planet 9 orbits that entail confinements in TNOs angular orbital elements that compares to the confinement encountered in the angular orbital elements of observed TNOs. One of their criteria is to discard those orbital parameters of Planet 9 that lead to the generation of too many particles with perihelion distance q > 42 au in the range of 100 au < a < 200 au, due to the non-existence of such observed objects; namely, they apparently assign a null probability to planets with low a9 and high e9 (low values of q9) since these are prone to produce high-perihelion distance objects in that region.

Currently5 there are three objects (2013 UT15, 2014 SS349, and 2015 KE172, according to the MPC database) observed in more than one opposition with q > 42 au and 34 with q > 30 au, in that range of semimajor axis. We apply an Observational Bias Introducing Procedure (OBIP; Gomes et al. 2015) to our simulated particles in each model that belong to the range 100 au < a < 200 au and q > 30 au from 4.4 Gyr and determine the number of objects with q > 42 au among a sample of 34 objects that can be observed.

OBIP is a procedure that consists of assigning different sizes to the simulated objects and a certain albedo to obtain their visual magnitudes, thus determining observable objects up to a certain visual magnitude. Sizes are determined by a cumulative size distribution function that follows a power law:

Equation (1)

where N is the number of objects with radius greater than r, N0 is a scaling factor, R0 is the radius above which there is just one object, and γ is an empirical parameter obtained from observations. We consider a size distribution with three slopes6 (Fraser et al. 2010; Shankman et al. 2013; Fraser et al. 2014) γ = 3, γ = 5 and γ = 2, respectively for radii in the range r > 200 km, 50 km < r < 200 km and r < 50 km. The largest r (R0) is determined by associating it with the visual magnitude of 20.5, which is approximately the magnitude of the brightest TNO with 100 au < a < 200 au and q > 30 au. Albedos are taken as 0.25.

This collection of sizes is randomly associated to the simulated particles' orbits which for the last 108 year belong to the range 100 au < a < 200 au and q > 30 au. The mean longitudes are chosen randomly in the range 0°–360°. Since there are 34 real objects within the limits above, we determine the 34 brightest objects by OBIP and the number of them with q > 42 au. Another parameter that is considered by OBIP is the range of ecliptic latitude in which it will be applied, we consider a reasonable range of ±30°.

The mean and standard deviation of the number of objects with q > 42 au and 100 au < a < 200 au among the 34 brightest ones determined by 1000 realizations of OBIP are depicted for each model in Table 3. Although we can see some trend for a larger number of OBIP-determined objects with q > 42 au for Planet 9 with a smaller q9, this trend is not well defined as to place a low-perihelion Planet 9 as prohibitive or even unlikely (see also Figure 10). A typical example is Planet 9 with a9 = 1500 au and q9 = 60 au. OBIP determines an average of 3.56 objects with q > 42 au and standard deviation at 1.80, thus three objects is well within the range of statistically acceptable numbers. Most Planet 9 models yield statistically coherent results with respect to the ratio of observable detached to scattering objects, which suggests that orbital parameters of Planet 9 with low q9 should not be discarded as suggested in Brown & Batygin (2016).

Figure 10.

Figure 10. Average of the number of observable objects by 1000 realizations of OBIP, with q > 42 au among the 34 brightest ones with q > 30 au and 100 au < a < 200 au, for models with i9 = 30° and ω9 = 0° as a function of the perihelion distance of Planet 9. The bars represent standard deviations of the mean values.

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Table 3.  Mean and Standard Deviation of the Number of Objects with q > 42 au Among the 34 Brightest Ones with q > 30 au, in the Range 100 au < a < 200 au

Model Number of Objects With q > 42 au
  Mean Std
a1500-10-0-100-5 5.69 2.25
a1500-30-0-60-5 3.56 1.80
a1500-30-0-100-5 2.14 1.43
a1500-30-0-200-5 2.75 1.57
a1500-30-0-300-5 2.76 1.62
a1500-30-90-60-5 5.30 2.13
a1500-60-0-100-5 5.79 2.18
a700-10-0-100-3 9.69 2.93
a700-30-0-60-3 5.23 2.31
a700-30-0-100-3 3.67 1.89
a700-30-0-200-3 4.31 2.05
a700-30-0-300-3 1.82 1.32
a700-30-90-60-3 3.35 1.77
a700-60-0-100-3 8.04 2.59

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4.2. The Influence of Planet 9 on the Classical Kuiper Belt

4.2.1. Cold Classical Kuiper Belt

In order to analyze the influence of Planet 9 on the Cold Classical Kuiper Belt Objects (CCKBOs), we performed new numerical integrations for the models a700-30-0-60-3 and a1500-30-0-60-5. Both simulations were done with an integration time of 4.5 Gyr and initially considering the current orbital configuration of the four giant planets, the respective external perturber and a disk composed of 2000 test particles with 42.5 au < a < 46 au, 0 < e < 0.01, 0° < i < 0fdg6 and remaining orbital elements randomly distributed between 0° and 360°. We chose a conspicuously cold disk in order to check not only the compatibility of Planet 9 with the Cold Classical Kuiper Belt (CCKB) but also whether Planet 9 could be responsible for some of the excitation we currently find there.

Both tested models present similar results (see, e.g., Figure 11). Planet 9 leads to the scattering of particles both inwards and outwards, although mostly outwards. They are however destabilized once they enter the secular resonance region; therefore, the main effect is to drive the semimajor axes of the particles to higher values. The eccentricities as well as the inclinations were excited within the values of the observed cold population. Assuming a local formation, the original external borders of the cold disk are unknown. Thus, from the data of the original simulations, we can obtain cold disks with different external edges by restricting the initial semimajor axes of the particles; the best fit is then determined according to the final distribution of the semimajor axes of the particles in the interval 42 au < a < 46 au, when compared to that of the actual cold population. Figures 12 and 13 show, for each model, the histograms in semimajor axis at 4.5 Gyr for the original disk and that corresponding to the best fit. These figures suggest that the fuzziness of the observed outer border of the CCKB could be a signature of the perturbation of a low-perihelion Planet 9.

Figure 11.

Figure 11. Eccentricity and inclination as a function of the semimajor axis for real CCKBOs and simulated particles at 4.5 Gyr considering the model a700-30-0-60-3, in red and blue, respectively. The simulated particles had initially semimajor axes between 42.5 and 46 au in almost circular and low-inclination orbits.

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Figure 12.

Figure 12. Distribution of semimajor axes for actual CCKBOs and simulated particles at 4.5 Gyr for model a700-30-0-60-3, in red and blue, respectively. The top panel shows the results for the full set of particles and the bottom one for the best fit in the truncation of the initial outer edge of the disk, at 44.6 au.

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Figure 13.

Figure 13. Same as Figure 12 for the model a1500-30-0-60-5, where the best fit of the outer edge of the disk is at 44.6 au.

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The eccentricities of the simulated particles always have low values, so they do not compare very nicely with the real eccentricity distribution mainly for higher semimajor axes (a > 44.5 au). Thus, the peculiar distribution of the eccentricities of the CCKB would not be explained by the perturbations of such a planet with low perihelion. Some other mechanism must have acted to excite the eccentricities of these particles (e.g., a temporary excited Neptune in a planetary instability migration model (Gomes et al. 2018)). The inclinations, on the other hand, are kept within the range of the observed inclinations in the CCKB.

Possibly the only inconsistency produced by a low-perihelion Planet 9 on the CCKB refers to a dearth of simulated particles just past the 4:7 resonance. This is likely produced by the outward scattering of particles by Planet 9 and the barrier effect of the 4:7 resonance that must capture some outward migrating particles.

4.2.2. Hot Classical Kuiper Belt

We also analyze the influence of Planet 9 on the Hot Classical Kuiper Belt objects. For this, we performed simulations considering the actual Classical population (and resonant objects) of the Kuiper Belt for the model a700-30-0-60-3 and evolve the system by 4.5 Gyr. The orbital elements of the Kuiper Belt and the four known giant planets were taken for the same date from the JPL Small-Body Database.7 The results show that a planet with such low-perihelion would excessively clean objects with higher eccentricities (Figure 14). These results led us to consider perihelion distances a little higher for Planet 9.

Figure 14.

Figure 14. Eccentricity and inclination as a function of the semimajor axis for actual CKBOs (in brown) and their configuration after 4.5 Gyr under the influence of Planet 9 under the model a700-30-0-60-3 (in blue).

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We thus performed numerical integrations considering a theoretical distribution of particles uniformly and randomly distributed in the ranges 38.5 au < a < 46.5 au, 0 < e < 0.25 and 0° < i < 20° under the influence of the known giant planets and compared the results with two other models that additionally consider a Planet 9 with a low-perihelion but larger than 60 au, namely, a9 = 700 au and q9 = 70 au and, a9 = 1500 au and q9 = 90 au. The results at 4.5 Gyr are presented in Figures 1517 as the ratio of the number of surviving objects to the number of initial objects in the grid of the plane a − e for objects with any inclination and for objects with i < 5°.

Figure 15.

Figure 15. Ratio of the number of surviving objects at the end of the integration time to the number of initial objects as function of the semimajor axis and eccentricity from an initially uniform distribution under the influence of the known planets. The upper panel considers all inclinations and the lower panel considers only cold objects (i < 5°).

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Figure 16.

Figure 16. Same as Figure 15 adding a planet with a9 = 700 au and q9 = 70 au.

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Figure 17.

Figure 17. Same as Figure 15 adding a planet with a9 = 1500 au and q9 = 90 au.

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Figure 15 shows that a model without an additional external planet tends to preserve more hot and cold objects at the lower right end of the plane a − e. This is already well known since this is the region that keeps objects far from close encounters with Neptune. Moreover, the region between roughly 40 and 42 au is also depleted due to the ν8 secular resonance.

Now comparing Figures 1517, we notice that the model with an external perturber with a9 = 1500 au and q9 = 90 au preserves the characteristics of the theoretical Kuiper Belt at 4.5 Gyr seen in the model considering only the known giant planets. The hot objects show a good approximation and most objects in the 3:5 and 4:7 MMRs (corresponding to a = 42.3 au and a = 43.7 au) survived until the end of the integration. The model that considers a planet with a9 = 700 au and q9 = 70 au has a smaller fraction of hot objects compared to the previous one and does not keep most objects in MMR. The right comparison of the distribution of TNOs in the Kuiper Belt from simulations with the observed ones makes sense only if the right initial conditions are considered. For instance, the initial distribution of objects after the stabilization of the giant planets8 might have concentrated most objects in smaller semimajor axes. Planet 9 could thus shift the semimajor axes outwards toward a distribution similar to our present one. Apart from this speculation, these last results show that a Planet 9 with a perihelion distance as low as 90 au does not significantly affect the Classical Kuiper Belt.

5. Conclusions

An external perturber was proposed to explain the confinements in the orbital elements Ω, ω, and ϖ of TNOs with q > 30 au and a > 250 au. Brown & Batygin (2016) claimed that good orbits for Planet 9 should have q9 > 200 au, to explain such confinements, where lower perihelia than that above were assigned a null probability arguing that these parameters produce objects with q > 42 au in the region 100 au < a < 200 au, where no object with such perihelion distance had been observed previously. On the other hand, Gomes et al. (2017) explain the inclination of the solar equator in relation to the invariable plane of known planets showing that parameters of the Planet 9 similar to those found by Batygin & Brown (2016a) and Brown & Batygin (2016) are compatible although with slightly higher eccentricities.

In this way, we considered perihelion distances for Planet 9 lower than those indicated by Brown & Batygin (2016) and we tested their influence on the TNOs with a ≥ 250 au and q ≥ 40 au, since these objects would not be greatly influenced by Neptune. In this region, there are currently nine objects whose Ω exhibit a large confinement (210fdg5), while the confinement in ω is 131fdg7, and we assume two confinements in the observational sample of ϖ.

Through statistical analysis, we tested the influence of a Planet 9 with a9 = 700 au and a9 = 1500 au and perihelion distances ranging from 60 to 300 au. Our results show that smaller perihelion distances (q9 = 60 au or q9 = 100 au) produce narrower confinements. Such confinements are generally best reproduced in ϖ, and interestingly, in several models, there are two confinements in this angular element, as assumed in the observational data, being shepherded by Planet 9. Models with high q9 are generally associated with random distributions in Ω and ω.

We also verified that a planet with low-perihelion roughly yielded the current observed ratio between the number of scattered and detached with q > 42 au objects in the interval 100 au < a < 200 au by applying an observational bias to the particles of our models. We saw that several of our models are compatible with this ratio. Likewise, we verified whether the existence of a Planet 9 with such low-perihelion would destroy the Classical Kuiper Belt. Integrations considering the most extreme cases of perihelion distance of Planet 9 from our models on an initially cold disk show that the signature due to the external perturber would be that of moving the semimajor axes of the objects to larger values and the sparseness of particles immediately past the 4:7 MMR. However, when we considered also the hot objects, a Planet 9 with a perihelion at 60 au would considerably deplete the region with a particularly important depletion for the resonant objects.

This motivated us to perform other runs with low-perihelion distances but larger than 60 au. For this, we considered a theoretical Classical Kuiper Belt and showed that a Planet 9 with q9 = 90 au produces signatures similar to those produced without an additional external planet. Thus, we concluded that planets with perihelion distances as small as 90 au should not be discarded in principle. They produce better confinements while preserving the Classical Kuiper Belt and the ratio between the number of detached to scattering objects in the region 100 au < a < 200 au.

A last remark is that although a very low-perihelion distance for Planet 9 (∼60–70 au) seems to excessively empty the Kuiper Belt region, it may not, depending on the initial conditions of the particles just after the stabilization of the planets. If these objects were much more concentrated on smaller semimajor axes, a low-perihelion Planet 9 could drift these objects outward so as to populate the Kuiper Belt conveniently. This problem is the subject of a following work by the authors.

The numerical simulations were done by the Lobo Carneiro supercomputer in the High Performance Computing Center of NACAD/COPPE/UFRJ. J.C. thanks support from the Coordination for the Improvement of Higher Education Personnel (CAPES), and R.G. acknowledges the Brazilian CNPq grant through process 307009/2014-9.

Footnotes

  • These numbers are taken from that paper's Figures 2 and 3  and their empirical expressions of e9 as a function of a9.

  • As of 2018 May.

  • For one of the cases (planet with a9 = 700 au and orbital inclination at 10°), we considered 20000 particles since there were too few particles in the end of the integration to perform a reliable statistics.

  • As of 2018 May.

  • In fact, OBIP never reaches the slope associated to the smallest sizes since only brighter objects are needed to be considered.

  • In a Nice model scenario; however, a smoother migration scenario could also work in this case.

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10.3847/1538-3881/aad77a