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JPL Small-Body Database Browser
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(2012 GV11)
Classification: Apollo [NEO]          SPK-ID: 3602572
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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2156531559248489 1.6391e-06  
a 1.044955908920989 4.3537e-07 au
q .8196078693598584 1.3718e-06 au
i 5.403707604922408 3.02e-05 deg
node 164.6606610636764 6.5244e-05 deg
peri 217.5376790726015 0.00016358 deg
M 42.50090822333423 0.0011918 deg
tp 2458554.438180823428
(2019-Mar-11.93818082)
0.0012629 TDB
period 390.1623658588517
1.07
0.00024384
6.676e-07
d
yr
n .9226927851115104 5.7665e-07 deg/d
Q 1.270303948482119 5.2926e-07 au
  Orbit Determination Parameters
   # obs. used (total)      82  
   data-arc span      666 days (1.82 yr)  
   first obs. used      2012-04-13  
   last obs. used      2014-02-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .5216  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:50:08  

Additional Information
 Earth MOID = .0749562 au 
 Jupiter MOID = 4.12806 au 
 T_jup = 5.851 
[ 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 22.3   n/a E2014B58  

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