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(2016 VQ)
Classification: Apollo [NEO]          SPK-ID: 3763270
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 2457690.5 (2016-Oct-29.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6575927055969254 0.00088469  
a 2.475856574767386 0.0060152 au
q .8477513510961642 0.00013071 au
i 2.656016092259335 0.002732 deg
node 229.7574462543625 0.00022553 deg
peri 229.0285068935618 0.002587 deg
M 347.9764535688462 0.046723 deg
tp 2457738.024410096531
(2016-Dec-15.52441010)
0.011484 TDB
period 1422.940205929687
3.90
5.1856
0.0142
d
yr
n .2529972788032872 0.000922 deg/d
Q 4.103961798438608 0.0099707 au
  Orbit Determination Parameters
   # obs. used (total)      54  
   data-arc span      17 days  
   first obs. used      2016-10-25  
   last obs. used      2016-11-11  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .47863  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:22:31  

Additional Information
 Earth MOID = .0011288 au 
 Jupiter MOID = 1.12218 au 
 T_jup = 3.140 
[ 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 26.0   n/a MPO397900  

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