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JPL Small-Body Database Browser
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212682 (2006 VT109)
Classification: Main-belt Asteroid          SPK-ID: 2212682
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 13 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1715004765243326 4.3873e-08  
a 2.434224324590002 1.85e-08 au
q 2.016753692955695 1.1258e-07 au
i 6.972055712640242 8.154e-06 deg
node 137.788856501524 3.6372e-05 deg
peri 265.2194970211882 4.6622e-05 deg
M 213.8369767905199 2.8618e-05 deg
tp 2459563.715165340354
(2021-Dec-15.21516534)
0.00011386 TDB
period 1387.200778078711
3.80
1.5814e-05
4.33e-08
d
yr
n .259515425372385 2.9585e-09 deg/d
Q 2.85169495622431 2.1673e-08 au
  Orbit Determination Parameters
   # obs. used (total)      273  
   data-arc span      8498 days (23.27 yr)  
   first obs. used      1995-11-30  
   last obs. used      2019-03-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .57054  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-14 08:43:42  

Additional Information
 Earth MOID = 1.03953 au 
 Jupiter MOID = 2.57379 au 
 T_jup = 3.475 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 16.5   n/a MPO433390  

212682 (2006 VT109)          Discovered 2006-Nov-13 by CSS at Catalina
Reference: 20090409/Numbers.arcLast Updated: 2009-04-10

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