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JPL Small-Body Database Browser
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(2012 VE26)
Classification: Apollo [NEO]          SPK-ID: 3617078
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 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6332095866122524 0.0016834  
a 1.587013387108915 0.0046752 au
q .5821012963095685 0.00096832 au
i 3.57649333395055 0.015887 deg
node 44.57930402425818 0.00052259 deg
peri 94.72394201257006 0.047697 deg
M 335.0721766092984 0.13868 deg
tp 2456289.065134938372
(2012-Dec-27.56513494)
0.057872 TDB
period 730.2462109308777
2.00
3.2269
0.008835
d
yr
n .492984413491296 0.0021784 deg/d
Q 2.591925477908262 0.0076356 au
  Orbit Determination Parameters
   # obs. used (total)      26  
   first obs. used      2012-11-07  
   last obs. used      2012-11-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .49148  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:48:07  

Additional Information
 Earth MOID = .00115799 au 
 Jupiter MOID = 2.46126 au 
 T_jup = 4.132 
[ 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 28.4   n/a MPO244127  

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