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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.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3131429906374522 9.8139e-05  
a 1.157385156571142 9.5164e-05 au
q .7949581073230587 4.8223e-05 au
i 5.496932534419961 0.0019821 deg
node 348.1877260076836 0.00048903 deg
peri 105.523275740427 0.00089468 deg
M 357.9065564363572 0.084551 deg
tp 2459003.144685571577
(2020-Jun-02.64468557)
0.10714 TDB
period 454.7945893085906
1.25
0.056092
0.0001536
d
yr
n .7915661453828998 9.7627e-05 deg/d
Q 1.519812205819225 0.00012496 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.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .33643  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Feb-10 07:09:10  

Additional Information
 Earth MOID = .0100879 au 
 Jupiter MOID = 3.65994 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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