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(2020 GQ1)
Classification: Apollo [NEO]          SPK-ID: 54016475
[ 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 2458943.5 (2020-Apr-04.0) TDB
Reference: JPL 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6518941034272061 0.0029098  
a 2.21674023882505 0.016679 au
q .7716603483051833 0.00064418 au
i .3094198465658107 0.0010716 deg
node 272.0439763530938 0.10252 deg
peri 351.7516504164089 0.09871 deg
M 346.3769394673399 0.17221 deg
tp 2458989.118691033579
(2020-May-19.61869103)		 0.061806 TDB
period 1205.509491256852
3.30		 13.606
0.03725		 d
yr
n .2986289221370358 0.0033704 deg/d
Q 3.661820129344917 0.027552 au
   Orbit Determination Parameters
   # obs. used (total)      19  
   data-arc span      2 days  
   first obs. used      2020-04-03  
   last obs. used      2020-04-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .4668  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Apr-05 08:12:10  

Additional Information
 Earth MOID = .00462432 au 
 Jupiter MOID = 1.44766 au 
 T_jup = 3.337 
[ 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 26.782   .3592 1 autocmod 2.8

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