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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.


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Orbital Elements at Epoch 2456238.5 (2012-Nov-07.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5633238549216011 0.0070942  
a 1.846934256988678 0.026204 au
q .8065121315550529 0.00166 au
i 4.066983988024834 0.033894 deg
node 217.3741082467256 0.0427 deg
peri 257.8966398574674 0.030236 deg
M 339.7233624305572 0.52705 deg
tp 2456290.137953207325
(2012-Dec-28.63795321)		 0.24569 TDB
period 916.8020630132461
2.51		 19.511
0.05342		 d
yr
n .3926692734708633 0.0083566 deg/d
Q 2.887356382422303 0.040965 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.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      9  
   norm. resid. RMS      .47737  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-16 06:15:02  

Additional Information
 Earth MOID = .0203409 au 
 Jupiter MOID = 2.2713 au 
 T_jup = 3.799 
[ 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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