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105093 (2000 LE1)
Classification: Main-belt Asteroid          SPK-ID: 2105093
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | 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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1554012830576895 7.3994e-08  
a 3.163180775851269 4.5984e-08 au
q 2.671618424740564 2.4593e-07 au
i 18.11583265697712 6.7328e-06 deg
node 95.39066131457385 2.0579e-05 deg
peri 156.2953508071889 3.4951e-05 deg
M 204.9402085853104 3.6331e-05 deg
tp 2459885.577173727054
(2022-Nov-02.07717373)
0.00022308 TDB
period 2054.870444715136
5.63
4.4809e-05
1.227e-07
d
yr
n .1751935266409977 3.8203e-09 deg/d
Q 3.654743126961973 5.313e-08 au
  Orbit Determination Parameters
   # obs. used (total)      364  
   data-arc span      7472 days (20.46 yr)  
   first obs. used      2000-05-05  
   last obs. used      2020-10-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .61514  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 19:38:53  

Additional Information
 Earth MOID = 1.66556 au 
 Jupiter MOID = 1.48775 au 
 T_jup = 3.109 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 14.8   n/a MPO453507  

105093 (2000 LE1)          Discovered 2000-Jun-01 by Crni Vrh at Crni Vrh
Reference: 20051019/Numbers.arcLast Updated: 2005-10-26

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