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(2020 VS1)
Classification: Apollo [NEO]          SPK-ID: 54087654
[ 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6039430569271069 0.00077095  
a 2.498512172518939 0.0048781 au
q .9895530932782638 5.7699e-06 au
i 3.107506062582666 0.0028835 deg
node 234.9741304435512 0.0006325 deg
peri 196.2854941625967 0.00013912 deg
M 314.4408389223969 0.13415 deg
tp 2459183.055049020657
(2020-Nov-29.55504902)		 0.0029275 TDB
period 1442.515974679445
3.95		 4.2245
0.01157		 d
yr
n .2495639606902786 0.00073087 deg/d
Q 4.007471251759614 0.0078241 au
   Orbit Determination Parameters
   # obs. used (total)      38  
   data-arc span      11 days  
   first obs. used      2020-11-05  
   last obs. used      2020-11-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .50573  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-18 05:28:20  

Additional Information
 Earth MOID = .0100331 au 
 Jupiter MOID = 1.31964 au 
 T_jup = 3.186 
[ 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 27.178   .66976 6 autocmod 2.8

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