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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 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456749.5 (2014-Apr-02.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .05849051008492837 8.7739e-05  
q .9682357593647424 2.4803e-05 au
tp 2456831.677860236547
(2014-Jun-23.17786024)
0.030653 TDB
node 10.2890311179202 0.0010649 deg
peri 265.0072437475219 0.027529 deg
i 9.692909561435224 0.010893 deg
  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
 Jupiter MOID = 3.91387 au 
 T_jup = 5.928 
Orbit Covariance (6×6)
  e q tp node peri i
e 7.698087158060654E-9 -2.150826578550996E-9 -2.661034437527327E-6 -9.336126494568734E-8 -2.379483485860207E-6 9.540641187340728E-7
q -2.150826578550996E-9 6.151973656242822E-10 7.267992637397413E-7 2.621568126099558E-8 6.470687167275706E-7 -2.686856200021254E-7
tp -2.661034437527327E-6 7.267992637397413E-7 .00093962805668535 3.210913594558071E-5 .0008435387741060422 -.0003271617093405782
node -9.336126494568734E-8 2.621568126099558E-8 3.210913594558071E-5 1.13397691591245E-6 2.868516552066577E-5 -1.159620334606151E-5
peri -2.379483485860207E-6 6.470687167275706E-7 .0008435387741060422 2.868516552066577E-5 .000757827226263064 -.0002921161893847979
i 9.540641187340728E-7 -2.686856200021254E-7 -.0003271617093405782 -1.159620334606151E-5 -.0002921161893847979 .0001186524065908954

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  

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Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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