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97815 (2000 OA48)
Classification: Main-belt Asteroid          SPK-ID: 2097815
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 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2500038856648362 3.9454e-08  
a 2.332631092514561 1.0288e-08 au
q 1.749464255563309 9.2293e-08 au
i 24.48408208555858 5.6562e-06 deg
node 346.9481435894926 9.2927e-06 deg
peri 307.3618053088051 1.3897e-05 deg
M 236.7317239382085 1.3204e-05 deg
tp 2459446.070406678012
(2021-Aug-19.57040668)
4.9483e-05 TDB
period 1301.270298642588
3.56
8.6089e-06
2.357e-08
d
yr
n .2766527449182016 1.8303e-09 deg/d
Q 2.915797929465814 1.286e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1290  
   data-arc span      7748 days (21.21 yr)  
   first obs. used      1999-02-10  
   last obs. used      2020-04-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52048  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-May-20 17:32:37  

Additional Information
 Earth MOID = .812943 au 
 Jupiter MOID = 2.61374 au 
 T_jup = 3.411 
[ 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 14.5   n/a MPO502713  
diameter diameter 3.605 km 0.042 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.164   0.017 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

97815 (2000 OA48)          Discovered 2000-Jul-31 by LINEAR at Socorro
Reference: 20050224/Numbers.arcLast Updated: 2005-02-28

[ show close-approach data ]
Alternate Designations
 2000 OA48 = 1999 CE101 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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