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JPL Small-Body Database Browser
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(2006 VX2)
Classification: Aten [NEO]          SPK-ID: 3358222
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2905373365364673 3.8753e-06  
a .9341615546193215 7.9083e-08 au
q .6627527446454582 3.6761e-06 au
i 9.817424862910732 7.0347e-05 deg
node 47.2725232145916 2.1168e-05 deg
peri 126.5409311300473 0.00016244 deg
M 193.2670609061257 0.00079056 deg
tp 2458753.239131503300
(2019-Sep-26.73913150)
0.0007436 TDB
period 329.7853899776186
0.90
4.1878e-05
1.147e-07
d
yr
n 1.091619007210817 1.3862e-07 deg/d
Q 1.205570364593185 1.0206e-07 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 = .0227045 au 
 Jupiter MOID = 3.76642 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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