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(2020 VK6)
Classification: Apollo [NEO]          SPK-ID: 54087866
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 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6366494290257827 0.00067064  
a 2.588286094591736 0.004699 au
q .9404552303145343 2.8409e-05 au
i 1.967380893930716 0.0014145 deg
node 80.45765046516888 0.0043268 deg
peri 18.28913152930781 0.0022413 deg
M 311.6724935590566 0.13279 deg
tp 2459204.677899739423
(2020-Dec-21.17789974)
0.0049904 TDB
period 1520.956683250666
4.16
4.142
0.01134
d
yr
n .2366931313458512 0.00064458 deg/d
Q 4.236116958868937 0.0076907 au
  Orbit Determination Parameters
   # obs. used (total)      97  
   data-arc span      14 days  
   first obs. used      2020-11-12  
   last obs. used      2020-11-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .4183  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-26 05:21:10  

Additional Information
 Earth MOID = .00557674 au 
 Jupiter MOID = .974107 au 
 T_jup = 3.097 
[ 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 25.562   .55795 9 autocmod 2.8

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