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105192 (2000 OV37)
Classification: Main-belt Asteroid          SPK-ID: 2105192
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 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .187116816744611 6.1894e-08  
a 2.771298682735484 1.616e-08 au
q 2.252742094973487 1.6577e-07 au
i 10.62626082486309 5.0689e-06 deg
node 277.255549781729 2.8109e-05 deg
peri 80.97081203357519 3.1749e-05 deg
M 83.3982751244322 1.3913e-05 deg
tp 2458610.128595154105
(2019-May-06.62859515)
6.4198e-05 TDB
period 1685.09127478767
4.61
1.4739e-05
4.035e-08
d
yr
n .2136382790572349 1.8686e-09 deg/d
Q 3.289855270497482 1.9183e-08 au
  Orbit Determination Parameters
   # obs. used (total)      847  
   data-arc span      7122 days (19.50 yr)  
   first obs. used      2000-07-30  
   last obs. used      2020-01-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50917  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-24 02:18:33  

Additional Information
 Earth MOID = 1.27812 au 
 Jupiter MOID = 2.28536 au 
 T_jup = 3.287 
[ 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 14.9   n/a MPO453509  
diameter diameter 6.076 km 1.625 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2015ApJ...814..117N)  
geometric albedo albedo 0.033   0.024 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2012ApJ...759L...8M)  

105192 (2000 OV37)          Discovered 2000-Jul-30 by LINEAR at Socorro
Reference: 20051019/Numbers.arcLast Updated: 2005-10-26

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