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Sunday, February 13, 2022

2011 YO17 - Cometary Origin?

2011 YO17 - Backward simulation 

Simulation based on 100 clones:


Clones  Target

mean sd   mean sd
q 3.3457192543808 2.89972813116376e-07   3.34571929768682 2.8751e-07
e 0.184121058387053 7.17001427077198e-08   0.184121045157645 7.1351e-08
i 18.249168025204 9.19753172889254e-06   18.2491686171502 9.2211e-06
peri 165.624322571055 3.52571408153806e-05   165.624319088164 3.5024e-05
node 302.902335551023 2.30225190945596e-05   302.902339849507 2.2893e-05
tp 2458883.14050519 0.000193613119572893   2458883.14050091 0.00019246

the table above shows the orbital parameters distribution of the clones in comparison with the nominal (target) solution.

 

Simulation method

Mercury Integrator Package Version 6 by J. E. Chambers

 )---------------------------------------------------------------------
) Important integration parameters:
)---------------------------------------------------------------------
 algorithm (MVS, BS, BS2, RADAU, HYBRID etc) = BS
 start time (days)= 2459600.5
) stop time (days) = 102458000.5
 stop time (days) = -1d8
 output interval (days) = 100
 timestep (days) = 0.05
 accuracy parameter=1.d-12

...

 ejection distance (AU)= 100

If a clone comes into the solar system from a distance greater than 100 AU, it is considered to have a cometary origin.


Simulation Results

73 out of 100 clones have a cometary origin:

 

In the following plots, the time has been divided into 50 slots and it is shown vertically for graphical reasons.

The 27  clones that did not come from a distance greater than 100 AU are flagged as being on an asteroid-like orbit, while the other are considered to be on a cometary-like orbit (the more you look in the past, the less clones are found because they were "ejected" in the backward simulation).

 

Perihelium

Aphelium

Eccentricity


Orbital Period


Orbit specific energy


Inclination


Argument of perihelium


Ascending node



Longitude



Best wishes,

Alessandro Odasso


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