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(2012 VQ6)
Classification: Apollo [NEO]          SPK-ID: 3616700
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.


Orbital Elements at Epoch 2456237.5 (2012-Nov-06.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4956357639633069 0.001078  
a 1.508455153958893 0.0025349 au
q .7608108313220893 0.00034756 au
i .8398210936763031 0.0018879 deg
node 211.5159881321968 0.0024109 deg
peri 269.1374028250314 0.0014355 deg
M 331.9786429418223 0.087967 deg
tp 2456290.172471282639
(2012-Dec-28.67247128)
0.03258 TDB
period 676.7013325721908
1.85
1.7058
0.00467
d
yr
n .5319924502462762 0.001341 deg/d
Q 2.256099476595697 0.0037914 au
  Orbit Determination Parameters
   # obs. used (total)      29  
   data-arc span      5 days  
   first obs. used      2012-11-04  
   last obs. used      2012-11-09  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      8  
   norm. resid. RMS      .52385  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 07:10:44  

Additional Information
 Earth MOID = .004137 au 
 Jupiter MOID = 2.85426 au 
 T_jup = 4.385 
[ 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 27.0   n/a MPO244115  

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