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86762 (2000 GS75)
Classification: Main-belt Asteroid          SPK-ID: 2086762
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

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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.


Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 16 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1276330530411275 3.9678e-08  
a 2.310758255519988 1.0831e-08 au
q 2.015829124527982 9.3206e-08 au
i 2.70397923679 4.1833e-06 deg
node 60.79605530907475 0.0001065 deg
peri 219.7495572068275 0.00010864 deg
M 209.3620522703883 2.143e-05 deg
tp 2459537.361284712794
(2021-Nov-18.86128471)		 7.7473e-05 TDB
period 1283.010459247075
3.51		 9.0206e-06
2.47e-08		 d
yr
n .2805900742315563 1.9728e-09 deg/d
Q 2.605687386511994 1.2213e-08 au
   Orbit Determination Parameters
   # obs. used (total)      433  
   data-arc span      9177 days (25.13 yr)  
   first obs. used      1994-12-08  
   last obs. used      2020-01-23  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .57771  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 20:54:43  

Additional Information
 Earth MOID = 1.00029 au 
 Jupiter MOID = 2.50571 au 
 T_jup = 3.572 
[ show covariance matrix ]

[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 16.7   n/a MPO247948  

86762 (2000 GS75)          Discovered 2000-Apr-05 by LINEAR at Socorro
Reference: 20040830/Numbers.arcLast Updated: 2004-09-06

Alternate Designations
 2000 GS75 = 2001 UB135 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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