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97371 (2000 AO58)
Classification: Main-belt Asteroid          SPK-ID: 2097371
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 14 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1384486816155227 4.4251e-08  
a 2.171292474548195 9.8689e-09 au
q 1.870679894045292 9.3748e-08 au
i 4.034603244117085 6.4573e-06 deg
node 324.5102758850036 6.023e-05 deg
peri 75.84385925912301 6.5183e-05 deg
M 198.3560490335211 2.5779e-05 deg
tp 2459525.226350448031
(2021-Nov-06.72635045)
8.5265e-05 TDB
period 1168.627004177006
3.20
7.9674e-06
2.181e-08
d
yr
n .3080538090539218 2.1002e-09 deg/d
Q 2.471905055051098 1.1235e-08 au
  Orbit Determination Parameters
   # obs. used (total)      729  
   data-arc span      13242 days (36.25 yr)  
   first obs. used      1984-01-26  
   last obs. used      2020-04-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52513  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 17:30:58  

Additional Information
 Earth MOID = .883341 au 
 Jupiter MOID = 2.91354 au 
 T_jup = 3.673 
[ 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 16.1   n/a MPO359433  
diameter diameter 3.868 km 0.112 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.057   0.006 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

97371 (2000 AO58)          Discovered 2000-Jan-04 by LINEAR at Socorro
Reference: 20050224/Numbers.arcLast Updated: 2005-02-28

Alternate Designations
 2000 AO58 = 1997 EF19 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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