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(2015 VM64)
Classification: Apollo [NEO]          SPK-ID: 3733853
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 .6202772846134578 0.00051717  
a 1.886717604451484 0.0022752 au
q .7164295319299098 0.00011181 au
i 16.3097170978266 0.01115 deg
node 46.03832624100892 0.0011396 deg
peri 76.71960033620101 0.0037971 deg
M 254.7839226452676 1.1061 deg
tp 2459277.154911812656
(2021-Mar-03.65491181)
3.4087 TDB
period 946.583172044822
2.59
1.7122
0.004688
d
yr
n .380315233390768 0.00068794 deg/d
Q 3.057005676973059 0.0036865 au
  Orbit Determination Parameters
   # obs. used (total)      91  
   data-arc span      4 days  
   first obs. used      2015-11-07  
   last obs. used      2015-11-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .48181  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:30:53  

Additional Information
 Earth MOID = .0124379 au 
 Jupiter MOID = 2.30516 au 
 T_jup = 3.665 
[ 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 26.1   n/a MPO361299  

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