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JPL Small-Body Database Browser
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35756 (1999 GX58)
Classification: Main-belt Asteroid          SPK-ID: 2035756
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1596473433566328 5.1874e-08  
a 2.548882361314865 1.4243e-08 au
q 2.141960063802366 1.3138e-07 au
i 9.248157432385074 5.7304e-06 deg
node 126.7442888207734 2.6347e-05 deg
peri 170.7443866717135 3.0687e-05 deg
M 238.7449735936785 1.8835e-05 deg
tp 2459101.134027222751
(2020-Sep-08.63402722)
8.0397e-05 TDB
period 1486.356938278596
4.07
1.2458e-05
3.411e-08
d
yr
n .2422029263152154 2.0301e-09 deg/d
Q 2.955804658827365 1.6517e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1529  
   data-arc span      13623 days (37.30 yr)  
   first obs. used      1982-01-19  
   last obs. used      2019-05-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50724  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-30 03:55:28  

Additional Information
 Earth MOID = 1.12605 au 
 Jupiter MOID = 2.26541 au 
 T_jup = 3.405 
[ 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 13.8   n/a MPO385042  
diameter diameter 5.107 km 0.137 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.270   0.050 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

35756 (1999 GX58)          Discovered 1999-Apr-12 by LINEAR at Socorro
Reference: 20020227/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1999 GX58 = 1982 BF10 = 2000 MO5 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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