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97599 (2000 EH57)
Classification: Main-belt Asteroid          SPK-ID: 2097599
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 20 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .03033000475751688 7.043e-08  
a 3.188504678911012 2.7622e-08 au
q 3.091797316830276 2.2764e-07 au
i 21.71022934613147 1.0627e-05 deg
node 352.8204027919857 1.1959e-05 deg
peri 310.47863456218 0.00013323 deg
M 74.89296669326899 0.00013103 deg
tp 2458567.869086654835
(2019-Mar-25.36908665)
0.00075816 TDB
period 2079.596198160181
5.69
2.7024e-05
7.399e-08
d
yr
n .1731105299762002 2.2495e-09 deg/d
Q 3.285212040991748 2.846e-08 au
  Orbit Determination Parameters
   # obs. used (total)      689  
   data-arc span      7907 days (21.65 yr)  
   first obs. used      1998-12-12  
   last obs. used      2020-08-05  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .58212  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-25 08:50:05  

Additional Information
 Earth MOID = 2.10573 au 
 Jupiter MOID = 1.84413 au 
 T_jup = 3.086 
[ 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 13.9   n/a MPO400895  
diameter diameter 9.547 km 0.169 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.059   0.008 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

97599 (2000 EH57)          Discovered 2000-Mar-08 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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