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(2015 GE1)
Classification: Apollo [NEO]          SPK-ID: 3715510
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 .4455082433717638 0.00021575  
a 1.731237135643036 0.00064691 au
q .9599567204827433 1.4805e-05 au
i 11.09517673990231 0.003819 deg
node 200.5760877160096 8.2286e-05 deg
peri 34.08750250251244 0.0005441 deg
M 79.69732553995415 0.44744 deg
tp 2458816.306409902910
(2019-Nov-28.80640990)
0.93086 TDB
period 832.019041864958
2.28
0.46635
0.001277
d
yr
n .4326824049520134 0.00024252 deg/d
Q 2.50251755080333 0.00093511 au
  Orbit Determination Parameters
   # obs. used (total)      110  
   data-arc span      4 days  
   first obs. used      2015-04-11  
   last obs. used      2015-04-15  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .32448  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:34:30  

Additional Information
 Earth MOID = .00803755 au 
 Jupiter MOID = 2.51732 au 
 T_jup = 4.019 
[ 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 25.7   n/a MPO337001  

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