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229896 (2009 VE3)
Classification: Main-belt Asteroid          SPK-ID: 2229896
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

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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 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1187100597842201 6.1688e-08  
a 2.15335562896516 1.1667e-08 au
q 1.897730653514019 1.3441e-07 au
i 3.674751078651052 5.4053e-06 deg
node 119.3283270920089 7.6297e-05 deg
peri 218.981322283307 7.8162e-05 deg
M 189.2079598545249 1.8767e-05 deg
tp 2459548.066906083825
(2021-Nov-29.56690608)
6.1907e-05 TDB
period 1154.176072973149
3.16
9.3804e-06
2.568e-08
d
yr
n .311910815368614 2.535e-09 deg/d
Q 2.408980604416302 1.3052e-08 au
  Orbit Determination Parameters
   # obs. used (total)      261  
   data-arc span      9600 days (26.28 yr)  
   first obs. used      1993-10-21  
   last obs. used      2020-02-02  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .58047  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-25 06:35:27  

Additional Information
 Earth MOID = .889911 au 
 Jupiter MOID = 2.91298 au 
 T_jup = 3.691 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 17.5   n/a MPO454655  

229896 (2009 VE3)          Discovered 2009-Nov-10 by Mayhill at Mayhill
Reference: 20091231/Numbers.arcLast Updated: 2010-01-04

Alternate Designations
 2009 VE3 = 2001 BF39 = 2006 WK150 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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