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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.


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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1337280344584919 6.8383e-05  
a 1.11210659839123 6.8671e-05 au
q .9633867688800516 1.6565e-05 au
i 8.999058674854613 0.0027854 deg
node 20.00712713713461 0.00012872 deg
peri 224.6598318265585 0.00024929 deg
M 8.580027849275602 0.00084036 deg
tp 2458990.290505256000
(2020-May-20.79050526)
0.0019391 TDB
period 428.3690184234585
1.17
0.039677
0.0001086
d
yr
n .8403969113474187 7.784e-05 deg/d
Q 1.260826427902409 7.7854e-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 = .00387833 au 
 Jupiter MOID = 3.73685 au 
 T_jup = 5.584 
[ 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 26.25   .46714 6 autocmod 2.8

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