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(2012 VB26)
Classification: Apollo [NEO]          SPK-ID: 3617075
[ 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.


Orbital Elements at Epoch 2456238.5 (2012-Nov-07.0) TDB
Reference: JPL 6 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5637732378805165 0.0070976  
a 1.848597212825112 0.026272 au
q .8064075766138005 0.00166 au
i 4.066807767064225 0.0339 deg
node 217.3721924305979 0.042721 deg
peri 257.8957843546323 0.030141 deg
M 339.7561022591473 0.52692 deg
tp 2456290.124219874982
(2012-Dec-28.62421987)		 0.24559 TDB
period 918.0405568582331
2.51		 19.571
0.05358		 d
yr
n .3921395381833794 0.0083597 deg/d
Q 2.890786849036424 0.041084 au
   Orbit Determination Parameters
   # obs. used (total)      18  
   data-arc span      1 day  
   first obs. used      2012-11-06  
   last obs. used      2012-11-07  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      9  
   norm. resid. RMS      .47327  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 07:11:35  

Additional Information
 Earth MOID = .0203368 au 
 Jupiter MOID = 2.26796 au 
 T_jup = 3.797 
[ 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 25.5   n/a MPO244126  

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