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(2020 GE)
Classification: Apollo [NEO]          SPK-ID: 54016433
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.


Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .03952004863952935 9.7435e-06  
a 1.004467970973974 2.707e-06 au
q .9647713479042332 7.1984e-06 au
i 2.312178003935726 0.00053835 deg
node 183.2769538031114 0.0017252 deg
peri 116.5537537042723 0.0045411 deg
M 315.0395289407343 0.0037831 deg
tp 2459046.423070554552
(2020-Jul-15.92307055)
0.0036785 TDB
period 367.7075664497903
1.01
0.0014865
4.07e-06
d
yr
n .9790388690550844 3.9578e-06 deg/d
Q 1.044164594043715 2.814e-06 au
  Orbit Determination Parameters
   # obs. used (total)      40  
   data-arc span      18 days  
   first obs. used      2020-03-29  
   last obs. used      2020-04-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .60712  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Jan-20 05:19:51  

Additional Information
 Earth MOID = .00989736 au 
 Jupiter MOID = 3.95956 au 
 T_jup = 6.058 
[ 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 28.125   .45133 9 autocmod 2.8

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