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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.


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Orbital Elements at Epoch 2456237.5 (2012-Nov-06.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4956329593014818 0.0011669  
a 1.508448630210153 0.0027442 au
q .7608117716648282 0.00037617 au
i .839843127206748 0.0020439 deg
node 211.5163584337411 0.0025478 deg
peri 269.137029420021 0.0014478 deg
M 331.9784119685986 0.095232 deg
tp 2456290.172563750641
(2012-Dec-28.67256375)		 0.035273 TDB
period 676.6969426922388
1.85		 1.8466
0.005056		 d
yr
n .5319959013967759 0.0014517 deg/d
Q 2.256085488755478 0.0041043 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.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .51817  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:48:10  

Additional Information
 Earth MOID = .00413702 au 
 Jupiter MOID = 2.85428 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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