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(2018 VN6)
Classification: Apollo [NEO]          SPK-ID: 3836158
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 1 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6365999268852065 0.00067547  
a 2.269112515758198 0.0039939 au
q .8245956541322222 8.1365e-05 au
i 1.396768163768118 0.0010715 deg
node 231.5012669137386 0.00020795 deg
peri 234.9129371692841 0.00094275 deg
M 152.0803314336051 0.39696 deg
tp 2458473.084336817434
(2018-Dec-20.58433682)
0.015824 TDB
period 1248.482541798093
3.42
3.2962
0.009025
d
yr
n .2883500473154553 0.00076129 deg/d
Q 3.713629377384174 0.0065364 au
  Orbit Determination Parameters
   # obs. used (total)      32  
   data-arc span      5 days  
   first obs. used      2018-11-06  
   last obs. used      2018-11-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .48417  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Nov-10 21:12:46  

Additional Information
 Earth MOID = 9.52695E-5 au 
 Jupiter MOID = 1.46353 au 
 T_jup = 3.311 
[ 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 28.2   .35779 E2018-VF0 autocmod 2.6q

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