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Tuesday, July 17, 2018

Asteroid 2017 YE5 - binary object with cometary origin?

This is an interesting asteroid discovered by the Morocco Oukaimeden Sky Survey on Dec. 21, 2017

This asteroid is an Apollo and PHA and immediately following its discovery it was suspected to have a cometary origin.

In June 2018, observations from NASA's Goldstone Solar System Radar showed that the asteroid could be a binary system and this was confirmed by the Arecibo Observatory in Puerto Rico and the Green Bank Observatory in West Virginia.

There are two questions:
  • how likely is this object to have a cometary origin based solely on its current orbital parameters and uncertainty?
  • is its  binary nature telling us something about its origin? is it more likely to have a cometary origin or not?
I tried myself to answer in a rough way the first question and I  am looking forward to reading the first scientific results regarding the second question.

Regarding the cometary origin, as a first step, I read data from JPL Small-Body Database Browser and I generated 100 clones to simulate their behaviour in the last 1e8 JD.

(2017 YE5)

Classification: Apollo [NEO, PHA]          SPK-ID: 3795078
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]

Orbital Elements at Epoch 2458200.5 (2018-Mar-23.0) TDB
Reference: JPL 38 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .7102764889674997 2.4274e-06
a 2.820304229389295 2.1688e-05 au
q .8171084435184766 5.6341e-07 au
i 6.209783873125096 2.5738e-05 deg
node 103.960295639342 1.8222e-05 deg
peri 110.7683468906294 3.1019e-05 deg
M 348.9948146835015 0.00012049 deg
tp 2458253.385574217192
(2018-May-14.88557422)
3.1167e-05 JED
period 1729.985108896518
4.74
0.019956
5.464e-05
d
yr
n .2080942767360745 2.4004e-06 deg/d
Q 4.823500015260113 3.7093e-05 au
Orbit Determination Parameters
   # obs. used (total)      292  
   data-arc span      213 days  
   first obs. used      2017-12-12  
   last obs. used      2018-07-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   fit RMS      .32615  
   data source      ORB  
   producer      Otto Matic  
   solution date      2018-Jul-14 06:51:38  

Additional Information
 Earth MOID = .0205924 au 
 Jupiter MOID = .420057 au 
 T_jup = 2.875 

Clone generation
I tried to generate clones that have the same orbital parameters (mean and sigma) shown above.

This table summarizes what has been achieved versus the intended nominal target:

clones_mean clones_sd                         target_mean       target_sd
q 0.81710847 5.6E-07 0.81710844 5.6E-07
e 0.71027634 2.43E-06 0.71027649 2.43E-06
i 6.20978289 2.6E−05 6.20978387 2.6E−05
peri 110.76834516 3.1E−05 110.76834689 3.1E−05
node 103.96029755 1.82E-05 103.96029564 1.8E−05
tp 2458253.38557146 3.1E−05 2458253.38557422 3.1E−05

Simulation Algorithm
Mercury 6 integrator by John Chambers  (1999): "A Hybrid Symplectic Integrator that Permits Close Encounters between Massive Bodies''. 
Monthly Notices of the Royal Astronomical Society, vol 304, pp793-799.

I used the general Bulirsch-Stoer algorithm with all planets from Mercury to Pluto plus asteroids Ceres, Pallas and Vesta.

I also used as usual an arbitrary threshold of 100 AU as ejection distance from the solar system.

)O+_06 Integration parameters  (WARNING: Do not delete this line!!)
) Lines beginning with `)' are ignored.
)---------------------------------------------------------------------
) Important integration parameters:
)---------------------------------------------------------------------
 algorithm (MVS, BS, BS2, RADAU, HYBRID etc) = BS
 start time (days)= 2458200.5
 stop time (days) = -1d8
 output interval (days) = 100
 timestep (days) = 0.05
 accuracy parameter=1.d-12
)---------------------------------------------------------------------
ejection distance (AU)= 100
radius of central body (AU) = 0.005
central mass (solar) = 1.0

Graphic tools
All plots below have been implemented in language R using the package ggplot2.

  R Core Team (2018). R: A language and environment for statistical
  computing. R Foundation for Statistical Computing, Vienna, Austria.
  URL https://www.R-project.org/.

Simulation Results
About 60% of the clones were ejected from the solar system in this backward simulation (i.e. they actually came from the outskirt of the solar system and they have a likely cometary origin).

This plot shows that the numer of clones is initially 100 and then as you go back in the past (from right to left) their number is decreasing due to ejection from the solar system:
This second plot below shows the density distribution of the arrival time in the solar system:
In the following plots the simulation time has been divided into 10 slots and for every slot we show the distribution of the maximum parameter achieved in that time slot by all clones (their number is shown in red):
Specific Energy
In this plot, by definition, a specific energy greater than 0 means clones travelling on a hyperbolic trajectory:

The hyperbolic clones had the following V-Infinity:
Orbital Period
Eccentricity
Inclination
Peri
ascending node
Footprint q-Q
We can get rid of the temporal dimension and plot the density graph showing where the clones (only those on elliptical orbits) have been most of the time in the plane q-Q:

Footprint e-i
same approach as above:
Footprint w-om
Analysis of close approaches










Kind Regards,
Alessandro Odasso

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