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JPL Small-Body Database Browser
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(2018 VR6)
Classification: Apollo [NEO]          SPK-ID: 3836165
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2972000128632502 0.00061174  
a 1.34264269190855 0.0011211 au
q .9436092666025803 3.3508e-05 au
i 13.76585588975905 0.022196 deg
node 48.20768227368227 1.7844e-05 deg
peri 46.16363458493796 0.01365 deg
M 80.69685664395598 0.08783 deg
tp 2458473.122352818651
(2018-Dec-20.62235282)
0.020906 TDB
period 568.2495563316375
1.56
0.71173
0.001949
d
yr
n .6335244717549757 0.00079348 deg/d
Q 1.74167611721452 0.0014543 au
  Orbit Determination Parameters
   # obs. used (total)      28  
   data-arc span      6 days  
   first obs. used      2018-11-06  
   last obs. used      2018-11-12  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .35198  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Nov-19 06:41:46  

Additional Information
 Earth MOID = .0206939 au 
 Jupiter MOID = 3.49519 au 
 T_jup = 4.818 
[ 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 27.4   .32488 E2018W27 autocmod 2.6q

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