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(2020 GF1)
Classification: Apollo [NEO]          SPK-ID: 54016465
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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1335541390486793 6.8485e-05  
a 1.1118753916753 6.8789e-05 au
q .963379831010692 1.6548e-05 au
i 9.000039386814358 0.0027847 deg
node 19.98013634196422 0.00015129 deg
peri 224.6032856678157 0.00019924 deg
M 176.7953581029133 0.014889 deg
tp 2458990.194339652660
(2020-May-20.69433965)
0.0018139 TDB
period 428.2354386305288
1.17
0.039741
0.0001088
d
yr
n .8406590569693587 7.8014e-05 deg/d
Q 1.260370952339908 7.7976e-05 au
  Orbit Determination Parameters
   # obs. used (total)      84  
   data-arc span      5 days  
   first obs. used      2020-04-03  
   last obs. used      2020-04-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .45314  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-18 07:43:33  

Additional Information
 Earth MOID = .00455755 au 
 Jupiter MOID = 3.73599 au 
 T_jup = 5.585 
[ 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 26.3   .46714 E2020H25 autocmod 2.8

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