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(2016 VY1)
Classification: Apollo [NEO]          SPK-ID: 3763338
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 .1283224776663787 2.2245e-06  
a 1.117768224266934 2.7237e-06 au
q .9743334362722521 3.0393e-07 au
i 10.6261209407272 0.00010893 deg
node 230.5094838933462 3.404e-05 deg
peri 202.7800344914604 0.00033108 deg
M 342.6253001008596 0.00377 deg
tp 2459021.332475381344
(2020-Jun-20.83247538)
0.0045963 TDB
period 431.6443553453838
1.18
0.0015777
4.32e-06
d
yr
n .834019941513988 3.0484e-06 deg/d
Q 1.261203012261615 3.0732e-06 au
  Orbit Determination Parameters
   # obs. used (total)      40  
   # delay obs. used      2  
   # Doppler obs. used      1  
   data-arc span      4 days  
   first obs. used      2016-11-06  
   last obs. used      2016-11-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .32898  
   source      ORB  
   producer      OSOD/JPL  
   solution date      2017-Jul-12 14:25:04  

Additional Information
 Earth MOID = .00597739 au 
 Jupiter MOID = 3.9049 au 
 T_jup = 5.559 
[ 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 24.7   n/a MPO389563  

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