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JPL Small-Body Database Browser
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(2012 VE77)
Classification: Apollo [NEO]          SPK-ID: 3617955
[ 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 2456247.5 (2012-Nov-16.0) TDB
Reference: JPL 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5548647413513554 0.00071733  
a 1.640151933087833 0.0021566 au
q .7300894549581269 0.00021663 au
i 8.103710680545541 0.0094155 deg
node 235.4313715584436 0.00080547 deg
peri 254.0716413153601 0.00084756 deg
M 337.0663525517396 0.055235 deg
tp 2456296.375946221431
(2013-Jan-03.87594622)		 0.021319 TDB
period 767.228182059187
2.10		 1.5132
0.004143		 d
yr
n .4692215541845518 0.00092544 deg/d
Q 2.550214411217539 0.0033532 au
   Orbit Determination Parameters
   # obs. used (total)      33  
   data-arc span      3 days  
   first obs. used      2012-11-14  
   last obs. used      2012-11-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      8  
   norm. resid. RMS      .65742  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-17 06:09:47  

Additional Information
 Earth MOID = .00104328 au 
 Jupiter MOID = 2.58758 au 
 T_jup = 4.097 
[ 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 26.3   n/a MPO244152  

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