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(2016 VB4)
Classification: Apollo [NEO]          SPK-ID: 3763550
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 2457703.5 (2016-Nov-11.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5581780594250936 0.00071578  
a 1.391592016797835 0.0015551 au
q .6148358853501672 0.00030899 au
i 5.993010592474977 0.0081942 deg
node 47.98870535252681 0.00030358 deg
peri 261.1975990613692 0.00069229 deg
M 35.37131667025491 0.077983 deg
tp 2457644.586470032901
(2016-Sep-13.08647003)
0.031131 TDB
period 599.6064830120105
1.64
1.0051
0.002752
d
yr
n .6003937752500734 0.0010064 deg/d
Q 2.168348148245502 0.0024232 au
  Orbit Determination Parameters
   # obs. used (total)      101  
   data-arc span      11 days  
   first obs. used      2016-11-08  
   last obs. used      2016-11-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .39886  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:22:17  

Additional Information
 Earth MOID = .00945561 au 
 Jupiter MOID = 3.12977 au 
 T_jup = 4.593 
[ 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 23.8   n/a MPO397901  

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