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(2013 GO3)
Classification: Aten [NEO]          SPK-ID: 3634156
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 2456389.5 (2013-Apr-07.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4206976324795985 0.0031421  
a .9811959994619263 0.00113 au
q .5684091654898404 0.0024311 au
i 20.85439706884971 0.27005 deg
node 193.2106428515659 0.021119 deg
peri 144.6293105733646 0.018065 deg
M 253.5952123605401 0.37691 deg
tp 2456494.427843840171
(2013-Jul-20.92784384)
0.19043 TDB
period 355.0030465777008
0.97
0.61326
0.001679
d
yr
n 1.014075804335965 0.0017518 deg/d
Q 1.393982833434012 0.0016054 au
  Orbit Determination Parameters
   # obs. used (total)      21  
   data-arc span      7 days  
   first obs. used      2013-04-04  
   last obs. used      2013-04-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .58146  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:46:16  

Additional Information
 Earth MOID = .136113 au 
 Jupiter MOID = 4.05438 au 
 T_jup = 6.039 
[ 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 23.0   n/a MPO259320  

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