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(2002 LG62)
Classification: Mars-crossing Asteroid          SPK-ID: 3365956
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5143137314898694 1.7987e-07  
a 3.129895830768336 8.131e-08 au
q 1.520147426871288 5.9701e-07 au
i 21.50413102276149 1.3162e-05 deg
node 93.50252743615117 3.1349e-05 deg
peri 84.94324615274488 4.1792e-05 deg
M 140.8689089449124 1.8516e-05 deg
tp 2458409.082038655460
(2018-Oct-17.58203866)
7.5471e-05 TDB
period 2022.52199025301
5.54
7.8813e-05
2.158e-07
d
yr
n .1779955925003145 6.9361e-09 deg/d
Q 4.739644234665384 1.2313e-07 au
  Orbit Determination Parameters
   # obs. used (total)      88  
   data-arc span      5666 days (15.51 yr)  
   first obs. used      2002-06-07  
   last obs. used      2017-12-11  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .53848  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-14 21:23:23  

Additional Information
 Earth MOID = .694455 au 
 Jupiter MOID = 1.57333 au 
 T_jup = 2.900 
[ 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 17.6   n/a MPO264924  

[ show close-approach data ]
Alternate Designations
 2002 LG62 = 2013 AB20 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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