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(2010 RV3)
Classification: Apollo [NEO]          SPK-ID: 3545480
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 2455442.5 (2010-Sep-03.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .879210839248953 0.033831  
a 2.150895065012327 0.44785 au
q .2598048097664075 0.018802 au
i 8.802147601979456 0.75711 deg
node 349.8716357289094 0.34757 deg
peri 128.3780625109467 0.47536 deg
M 341.6499993763076 6.4299 deg
tp 2455501.230114040130
(2010-Oct-31.73011404)
2.2449 TDB
period 1152.198383423947
3.15
359.86
0.9852
d
yr
n .3124461943178576 0.097585 deg/d
Q 4.041985320258246 0.84161 au
  Orbit Determination Parameters
   # obs. used (total)      12  
   data-arc span      1 day  
   first obs. used      2010-09-02  
   last obs. used      2010-09-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .60572  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:56:54  

Additional Information
 Earth MOID = .00682727 au 
 Jupiter MOID = 1.19926 au 
 T_jup = 3.025 
[ 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 23.168   .41408 7 autocmod 2.6i

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