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(2015 VE106)
Classification: Apollo [NEO]          SPK-ID: 3734647
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 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2221536916084003 0.00022269  
a 1.261112832592661 0.00035664 au
q .9809519612974746 3.4282e-06 au
i 9.389878443194368 0.0075321 deg
node 234.3798659965993 0.0016362 deg
peri 193.3799331795651 0.0044865 deg
M 65.81376336406919 0.48372 deg
tp 2458905.932138378415
(2020-Feb-26.43213838)
0.65494 TDB
period 517.2843557880637
1.42
0.21943
0.0006008
d
yr
n .6959421756560823 0.00029522 deg/d
Q 1.541273703887847 0.00043587 au
  Orbit Determination Parameters
   # obs. used (total)      43  
   data-arc span      23 days  
   first obs. used      2015-11-13  
   last obs. used      2015-12-06  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .47526  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:30:37  

Additional Information
 Earth MOID = .00243193 au 
 Jupiter MOID = 3.73312 au 
 T_jup = 5.073 
[ 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 24.3   n/a MPO361302  

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