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(2010 RC73)
Classification: Main-belt Asteroid          SPK-ID: 3546666
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters ]

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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 2455450.5 (2010-Sep-11.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3253705679607431 0.11175  
a 2.62379094639126 0.31842 au
q 1.77008659595368 0.090707 au
i 3.906120903681764 0.40422 deg
node 60.42096661532974 4.0869 deg
peri 4.030771705087385 19.001 deg
M 320.9690998852301 1.2209 deg
tp 2455618.805511002629
(2011-Feb-26.30551100)
32.759 TDB
period 1552.359381484473
4.25
282.59
0.7737
d
yr
n .2319050628957731 0.042216 deg/d
Q 3.47749529682884 0.42203 au
  Orbit Determination Parameters
   # obs. used (total)      8  
   data-arc span      3 days  
   first obs. used      2010-09-10  
   last obs. used      2010-09-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .3618  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-08 00:32:09  

Additional Information
 Earth MOID = .782714 au 
 Jupiter MOID = 1.87448 au 
 T_jup = 3.323 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 17.112   .37721 3 autocmod 2.6i
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters ]
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