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(2018 VM6)
Classification: Apollo [NEO]          SPK-ID: 3836169
[ 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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2244349017763284 0.0004019  
a 1.300267683784185 0.00069231 au
q 1.008442233891147 1.4359e-05 au
i 30.06116321168664 0.019917 deg
node 46.70543917022869 0.00068627 deg
peri 359.3443983883136 0.0025834 deg
M 150.6777687401826 0.40615 deg
tp 2458973.829887593568
(2020-May-04.32988759)		 0.42995 TDB
period 541.5612478774009
1.48		 0.43252
0.001184		 d
yr
n .6647447567767942 0.0005309 deg/d
Q 1.592093133677222 0.00084769 au
   Orbit Determination Parameters
   # obs. used (total)      120  
   data-arc span      19 days  
   first obs. used      2018-11-09  
   last obs. used      2018-11-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .43651  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Dec-02 06:24:28  

Additional Information
 Earth MOID = .0176054 au 
 Jupiter MOID = 3.81003 au 
 T_jup = 4.845 
[ 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 22.9   .41453 E2018X15 autocmod 2.6q

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