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(2008 GV3)
Classification: Apollo [NEO]          SPK-ID: 3408588
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 38 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6053685777105811 6.4214e-08  
a 2.397435714769403 1.2682e-08 au
q .9461034659668994 1.5036e-07 au
i 72.89110066582285 3.1778e-05 deg
node 208.6481657832163 6.0173e-06 deg
peri 72.89081985210873 2.1831e-05 deg
M 79.43291364708175 9.9935e-06 deg
tp 2458701.330803337554
(2019-Aug-05.83080334)
3.6014e-05 TDB
period 1355.872595546383
3.71
1.0758e-05
2.945e-08
d
yr
n .2655116721014109 2.1067e-09 deg/d
Q 3.848767963571908 2.0359e-08 au
  Orbit Determination Parameters
   # obs. used (total)      212  
   data-arc span      4228 days (11.58 yr)  
   first obs. used      2008-04-07  
   last obs. used      2019-11-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .39196  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-04 04:54:50  

Additional Information
 Earth MOID = .248361 au 
 Jupiter MOID = 2.78637 au 
 T_jup = 2.488 
[ 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 18.4   n/a MPO241934  

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