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(2016 VZ1)
Classification: Apollo [NEO]          SPK-ID: 3763339
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 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1384667727313061 0.0001896  
a 1.07204869954387 0.00029001 au
q .9236055759072372 4.6636e-05 au
i 24.00058315816023 0.023063 deg
node 224.1882158374079 0.00078811 deg
peri 250.6729969302874 0.06554 deg
M 18.70135561128099 0.39233 deg
tp 2458979.438427851426
(2020-May-09.93842785)
0.4333 TDB
period 405.4340300824512
1.11
0.16452
0.0004504
d
yr
n .887937304934143 0.00036031 deg/d
Q 1.220491823180504 0.00033017 au
  Orbit Determination Parameters
   # obs. used (total)      41  
   data-arc span      2 days  
   first obs. used      2016-11-06  
   last obs. used      2016-11-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .4393  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:22:25  

Additional Information
 Earth MOID = .0142916 au 
 Jupiter MOID = 3.90805 au 
 T_jup = 5.675 
[ 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 MPO389563  

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