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(2014 GA)
Classification: Apollo [NEO]          SPK-ID: 3666885
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 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .05888240545599754 8.7085e-05  
a 1.029796653842278 6.2342e-05 au
q .9691597497335077 3.1289e-05 au
i 9.651520286918975 0.010968 deg
node 10.10152539413837 0.00029228 deg
peri 264.2978702591054 0.026965 deg
M 246.9007819899633 0.16322 deg
tp 2459120.417548823455
(2020-Sep-27.91754882)
0.18395 TDB
period 381.7030598090674
1.05
0.034662
9.49e-05
d
yr
n .9431415094761788 8.5645e-05 deg/d
Q 1.090433557951049 6.6013e-05 au
  Orbit Determination Parameters
   # obs. used (total)      41  
   data-arc span      5 days  
   first obs. used      2014-04-01  
   last obs. used      2014-04-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .40467  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:41:48  

Additional Information
 Earth MOID = .0192986 au 
 Jupiter MOID = 3.91387 au 
 T_jup = 5.928 
[ 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 26.4   n/a MPO290440  

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