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97382 (2000 AS72)
Classification: Main-belt Asteroid          SPK-ID: 2097382
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .07821542284765749 3.9547e-08  
a 2.751165872020607 1.6606e-08 au
q 2.535982270016471 1.0876e-07 au
i 12.93639451190578 4.2175e-06 deg
node 92.60224228044119 1.7388e-05 deg
peri 164.1665187455676 3.151e-05 deg
M 349.6935345932955 2.4656e-05 deg
tp 2459048.217846874669
(2020-Jul-17.71784687)
0.000114 TDB
period 1666.761998124592
4.56
1.5091e-05
4.132e-08
d
yr
n .2159876457497021 1.9556e-09 deg/d
Q 2.966349474024743 1.7905e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1256  
   data-arc span      7546 days (20.66 yr)  
   first obs. used      1999-10-20  
   last obs. used      2020-06-17  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .4855  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Jun-24 01:03:12  

Additional Information
 Earth MOID = 1.52263 au 
 Jupiter MOID = 2.1128 au 
 T_jup = 3.304 
[ 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 14.2   n/a MPO474850  
diameter diameter 3.873 km 0.248 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.324   0.044 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

97382 (2000 AS72)          Discovered 2000-Jan-05 by LINEAR at Socorro
Reference: 20050224/Numbers.arcLast Updated: 2005-02-28

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