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(2020 GO1)
Classification: Apollo [NEO]          SPK-ID: 54016473
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 2 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .3600899213629951 0.00025934  
a 1.555993036300562 0.00062964 au
q .9956956262177246 6.406e-07 au
i 8.343941229697123 0.0045236 deg
node 192.205584284917 0.00015293 deg
peri 349.6111592492467 0.0016695 deg
M 34.65685565033201 0.022279 deg
tp 2458932.250958400817
(2020-Mar-23.75095840)
0.0024508 TDB
period 708.9406847406973
1.94
0.43031
0.001178
d
yr
n .5077998875627711 0.00030823 deg/d
Q 2.116290446383399 0.00085637 au
  Orbit Determination Parameters
   # obs. used (total)      29  
   data-arc span      3 days  
   first obs. used      2020-04-02  
   last obs. used      2020-04-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .34961  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-09 06:22:33  

Additional Information
 Earth MOID = .000296689 au 
 Jupiter MOID = 2.84523 au 
 T_jup = 4.354 
[ 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 27.633   .42834 2 autocmod 2.8

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