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(2016 VX1)
Classification: Apollo [NEO]          SPK-ID: 3763337
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 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5388666763872865 1.6467e-05  
a 1.200382801756757 1.7605e-05 au
q .5535365109816341 1.1665e-05 au
i 3.503569445115079 0.00015954 deg
node 54.40637960512402 0.00015643 deg
peri 102.7724904682831 0.00057401 deg
M 208.1595053971978 0.020063 deg
tp 2459203.111075858921
(2020-Dec-19.61107586)
0.031229 TDB
period 480.3724296342318
1.32
0.010568
2.893e-05
d
yr
n .7494185298563314 1.6487e-05 deg/d
Q 1.847229092531879 2.7092e-05 au
  Orbit Determination Parameters
   # obs. used (total)      21  
   # delay obs. used      1  
   # Doppler obs. used      1  
   data-arc span      9 days  
   first obs. used      2016-11-04  
   last obs. used      2016-11-13  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .47301  
   source      ORB  
   producer      OSOD/JPL  
   solution date      2017-Jul-07 16:04:01  

Additional Information
 Earth MOID = .00218418 au 
 Jupiter MOID = 3.14664 au 
 T_jup = 5.142 
[ 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 25.0   n/a MPO389563  

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