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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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 13 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1385311285139948 4.5673e-08  
a 2.171383197691809 1.0274e-08 au
q 1.870579032879236 9.6331e-08 au
i 4.034400628287964 6.9533e-06 deg
node 324.5110417510414 6.0599e-05 deg
peri 75.93950595248799 6.6268e-05 deg
M 75.01392387459757 2.6402e-05 deg
tp 2458356.975579328706
(2018-Aug-26.47557933)
8.5219e-05 TDB
period 1168.700248079594
3.20
8.295e-06
2.271e-08
d
yr
n .3080345029373882 2.1863e-09 deg/d
Q 2.472187362504382 1.1698e-08 au
  Orbit Determination Parameters
   # obs. used (total)      717  
   data-arc span      12810 days (35.07 yr)  
   first obs. used      1984-01-26  
   last obs. used      2019-02-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52975  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-13 06:48:11  

Additional Information
 Earth MOID = .882676 au 
 Jupiter MOID = 2.91301 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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