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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.


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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 .03951515489058529 1.1114e-05  
a 1.00446655613707 3.0683e-06 au
q .9647749045889007 8.2292e-06 au
i 2.311907065742262 0.00061413 deg
node 183.2760807924986 0.0019709 deg
peri 116.5561449102461 0.0051674 deg
M 315.037527349138 0.0043013 deg
tp 2459046.425017968784
(2020-Jul-15.92501797)
0.004183 TDB
period 367.70678955187
1.01
0.0016848
4.613e-06
d
yr
n .9790409375870855 4.486e-06 deg/d
Q 1.044158207685239 3.1896e-06 au
  Orbit Determination Parameters
   # obs. used (total)      37  
   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      .53434  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-18 07:43:33  

Additional Information
 Earth MOID = .00989753 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 28.116   .46308 8 autocmod 2.8

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