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Sunday, October 21, 2018

2011 DL12 = K11D12L -- Cometary Origin?

2011 DL12 is an outer main-belt asteroid.

I have downloaded the orbital parameters  from JPL Small-Body Database Browser:

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]

Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3332919522378502 1.7048e-05
a 3.813848977356317 0.00010804 au
q 2.542723806152901 1.7234e-05 au
i 13.48245115796516 0.00011571 deg
node 329.3312783932701 0.00010623 deg
peri 151.9591228706485 0.0023481 deg
M 48.29805632413862 0.016968 deg
tp 2458235.518528997214
(2018-Apr-27.01852900)
0.11275 TDB
period 2720.468266449358
7.45
0.1156
0.0003165
d
yr
n .1323301596419123 5.6232e-06 deg/d
Q 5.084974148559733 0.00014405 au
Orbit Determination Parameters
   # obs. used (total)      22  
   data-arc span      413 days (1.13 yr)  
   first obs. used      2010-01-15  
   last obs. used      2011-03-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   fit RMS      .85076  
   data source      ORB  
   producer      Otto Matic  
   solution date      2018-Oct-18 05:08:18  

Additional Information
 Earth MOID = 1.56728 au 
 Jupiter MOID = .136519 au 
 T_jup = 2.934 
(2011 DL12)
Classification: Outer Main-belt Asteroid          SPK-ID: 3558704

I generated 100 clones trying to achieve the same nominal orbital parameters and uncertainty as calculated by JPL.

The result (achieved vs target) is shown in this table:

Clones Target
mean sd mean sd
q 2.54272169 1.715e-05 2.54272381 1.723e-05
e 0.33329091 1.712e-05 0.33329195 1.705e-05
i 13.48245868 0.00011564 13.48245116 0.00011571
peri 151.95937755 0.00234384 151.95912287 0.0023481
node 329.33127117 0.00010601 329.33127839 0.00010623
tp 2458235.53032508 0.11307094 2458235.518529 0.11275

Backward Simulation

As shown below, I investigated what could have happened to the clones in the past going back to -100 million JD (about 280K years in the past).

As arbitrary threshold to declare that an object is likely to have a cometary origin, I set ejection distance = 100 AU
 
Algorithm: Bulirsch-Stoer

Non gravitational effects: not taken ito account.

Software: Mercury 6 

 ===>  reference for the package: J.E.Chambers (1999) ``A Hybrid
      Symplectic Integrator that Permits Close Encounters between
      Massive Bodies''. Monthly Notices of the Royal Astronomical
      Society, vol 304, pp793-799.


)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
 

Simulation Results

(all analysis and plots below are done with R version 3.5.1 (R: A Language and Environment for Statistical Computing) using many libraries including library ggplot and viridis).

Going back in the past, 77 out of 100 clones seem to have a cometary origin because they entered the solar system coming from a distance greater than 100 AU.

As the simulation is backward, this plot should be read from right to left: we can see that many of the initial 100 clones are slowly "ejected" from the solar system (i.e. they entered in the solar system):

This plot show the density distribution of the arrival time in the solar system:

It seems that the most of the clones arrived in the solar sytem about 35000 years ago.

Footprint plots
If we forget the temporal dimension, we can draw some "footprint" plots that show where the clones were for most of the time:






Time plots
In the following plots, we take again into consideration the temporal dimension.

We start defining 10 time slots.
We take the first time slot and consider the first clone: we calculate the mean (or min/max) of an orbital parameter. Thus, we have one value.
Then, we do the same calculation for the other clones in the first time slot and we draw the resulting boxplot showing the distribution of all values.
The number of clones contributing to each interval in written over the boxplot itself.
The process is repeated for every time slot.

minimum value of perihelium

In case of aphelium, we need to discard a couple of outliers in order to be able to see the boxplots that otherwise would be too much "compressed":

maximum value of aphelium 


maximum value of eccentricity:
mean value of inclination 
mean value of w
mean value of om


In the energy plot, clones with hyperbolic orbits have energy greater than 0

maximum value of energy 


For hyperbolic clones we can show the Vinfinity while for the other we can show the orbital period (in the latter case, we discard a few outliers to better see the boxplots):

maximum value of Vinfinity  
maximum value of orbital Period 

Analysis of close encounters






Kind Regards,
Alessandro Odasso

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