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(2010 RS80)
Classification: Apollo [NEO]          SPK-ID: 3545979
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 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3693950104619493 0.000302  
a 1.461349242830742 0.00061488 au
q .9215341239867186 5.359e-05 au
i 9.043079792254272 0.0057462 deg
node 348.4214323198793 0.00015056 deg
peri 310.8117909944234 0.0002363 deg
M 203.158259862364 1.3021 deg
tp 2459281.617969010459
(2021-Mar-08.11796901)
2.5112 TDB
period 645.2521424141005
1.77
0.40724
0.001115
d
yr
n .5579214330898951 0.00035213 deg/d
Q 2.001164361674766 0.00084201 au
  Orbit Determination Parameters
   # obs. used (total)      52  
   data-arc span      7 days  
   first obs. used      2010-09-11  
   last obs. used      2010-09-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .38204  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:56:42  

Additional Information
 Earth MOID = .00576576 au 
 Jupiter MOID = 3.26092 au 
 T_jup = 4.533 
[ 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 26.5   n/a MPO183448  

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