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(2017 SO10)
Classification: Apollo [NEO]          SPK-ID: 3781642
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3131036647340463 9.826e-05  
a 1.157397541091637 9.5172e-05 au
q .7950121294216717 4.8354e-05 au
i 5.497048610832547 0.0019821 deg
node 348.1860699461745 0.00049198 deg
peri 105.5225670402017 0.00090229 deg
M 156.2193004082973 0.10409 deg
tp 2459003.142130733999
(2020-Jun-02.64213073)
0.10716 TDB
period 454.8018890755881
1.25
0.056097
0.0001536
d
yr
n .7915534404039557 9.7634e-05 deg/d
Q 1.519782952761603 0.00012497 au
  Orbit Determination Parameters
   # obs. used (total)      54  
   data-arc span      34 days  
   first obs. used      2017-08-31  
   last obs. used      2017-10-04  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      6  
   norm. resid. RMS      .33164  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 19:36:56  

Additional Information
 Earth MOID = .01022 au 
 Jupiter MOID = 3.65983 au 
 T_jup = 5.387 
[ show covariance matrix ]

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

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 24.6   n/a MPO438038  

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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