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(2006 VX2)
Classification: Aten [NEO]          SPK-ID: 3358222
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]

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 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2905876074683227 3.8777e-06  
a .9342317069638725 7.5897e-08 au
q .6627555504161936 3.6764e-06 au
i 9.816788866147791 7.0334e-05 deg
node 47.26664818083484 2.1246e-05 deg
peri 126.5400493673472 0.00016197 deg
M 128.1950660948149 0.00087028 deg
tp 2459083.051049370763
(2020-Aug-21.55104937)
0.00078302 TDB
period 329.8225393109375
0.90
4.0192e-05
1.1e-07
d
yr
n 1.091496053459867 1.3301e-07 deg/d
Q 1.205707863511551 9.7952e-08 au
  Orbit Determination Parameters
   # obs. used (total)      81  
   data-arc span      3279 days (8.98 yr)  
   first obs. used      2006-11-11  
   last obs. used      2015-11-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .58176  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 09:07:40  

Additional Information
 Earth MOID = .0225698 au 
 Jupiter MOID = 3.76389 au 
 T_jup = 6.369 
[ 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 24.6   n/a MPO354418  

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