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(2016 VZ)
Classification: Apollo [NEO]          SPK-ID: 3763275
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 .3249203125621939 0.00020298  
a 1.034414264805605 9.8135e-05 au
q .6983120585661757 0.00014372 au
i 4.181369662442314 0.0033081 deg
node 44.11751440467414 0.00066673 deg
peri 107.8412120496696 0.00047552 deg
M 69.38875615217339 0.15608 deg
tp 2458926.432654543650
(2020-Mar-17.93265454)
0.15606 TDB
period 384.2732719665698
1.05
0.054684
0.0001497
d
yr
n .9368333065624156 0.00013332 deg/d
Q 1.370516471045034 0.00013002 au
  Orbit Determination Parameters
   # obs. used (total)      71  
   data-arc span      5 days  
   first obs. used      2016-11-05  
   last obs. used      2016-11-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .42616  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Feb-10 07:08:28  

Additional Information
 Earth MOID = .00785481 au 
 Jupiter MOID = 3.62518 au 
 T_jup = 5.871 
[ 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 25.9   n/a MPO397900  

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