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(2010 RP64)
Classification: Apollo [NEO]          SPK-ID: 3545907
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 2455451.5 (2010-Sep-12.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5206541690039566 0.001429  
a 2.101845275730215 0.0062604 au
q 1.007510770320008 3.0114e-06 au
i 6.403326414090904 0.012455 deg
node 169.8817922665997 0.0015893 deg
peri 160.1139393220177 0.0074827 deg
M 5.363486055584168 0.024297 deg
tp 2455434.917721826107
(2010-Aug-26.41772183)
0.0010992 TDB
period 1113.011217095687
3.05
4.9727
0.01361
d
yr
n .3234468749914228 0.0014451 deg/d
Q 3.196179781140422 0.0095199 au
  Orbit Determination Parameters
   # obs. used (total)      16  
   data-arc span      5 days  
   first obs. used      2010-09-10  
   last obs. used      2010-09-15  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .34564  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:56:45  

Additional Information
 Earth MOID = .015154 au 
 Jupiter MOID = 2.19819 au 
 T_jup = 3.554 
[ 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 27.2   n/a MPO183443  

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