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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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2905812615456316 3.8772e-06  
a .9342073644124643 7.5162e-08 au
q .6627442099162709 3.6753e-06 au
i 9.817026550383101 7.0334e-05 deg
node 47.26959652677478 2.1208e-05 deg
peri 126.5357427658454 0.000162 deg
M 269.8964306599287 0.00084388 deg
tp 2459083.047295923899
(2020-Aug-21.54729592)
0.00078307 TDB
period 329.8096484995481
0.90
3.9802e-05
1.09e-07
d
yr
n 1.09153871524924 1.3173e-07 deg/d
Q 1.205670518908658 9.7002e-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 = .0229019 au 
 Jupiter MOID = 3.76495 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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