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JPL Small-Body Database Browser
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(2010 RM82)
Classification: Apollo [NEO]          SPK-ID: 3545981
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 11 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4166524087569352 0.00042632  
a 1.183104939596225 0.0004672 au
q .6901614167012292 0.00023185 au
i 5.05426576658504 0.0057352 deg
node 170.6080294705983 0.0023846 deg
peri 83.10626321098083 0.001963 deg
M 299.7551342845582 1.5093 deg
tp 2458679.159443253042
(2019-Jul-14.65944325)
2.0172 TDB
period 470.0383880818696
1.29
0.27842
0.0007623
d
yr
n .7658948909877048 0.00045367 deg/d
Q 1.67604846249122 0.00066185 au
  Orbit Determination Parameters
   # obs. used (total)      42  
   data-arc span      7 days  
   first obs. used      2010-09-12  
   last obs. used      2010-09-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .36456  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:56:42  

Additional Information
 Earth MOID = .0043274 au 
 Jupiter MOID = 3.38209 au 
 T_jup = 5.262 
[ 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 25.9   n/a MPO187184  

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