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359445 (2010 MH96)
Classification: Main-belt Asteroid          SPK-ID: 2359445
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .0646376685107793 5.6367e-08  
a 2.989814148781254 5.5377e-08 au
q 2.796559532923494 1.7739e-07 au
i 6.300026218517829 1.6296e-05 deg
node 185.9971713992824 5.3832e-05 deg
peri 277.7979028010619 0.00014217 deg
M 147.2013797678609 0.00013066 deg
tp 2457828.399033516852
(2017-Mar-15.89903352)
0.00068954 TDB
period 1888.272707581106
5.17
5.2461e-05
1.436e-07
d
yr
n .1906504280629906 5.2968e-09 deg/d
Q 3.183068764639015 5.8956e-08 au
  Orbit Determination Parameters
   # obs. used (total)      122  
   data-arc span      5885 days (16.11 yr)  
   first obs. used      2002-03-11  
   last obs. used      2018-04-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .68655  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-May-07 06:50:57  

Additional Information
 Earth MOID = 1.82253 au 
 Jupiter MOID = 1.92224 au 
 T_jup = 3.244 
[ 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 16.3   n/a MPO446598  
diameter diameter 3.697 km 1.050 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.039   0.042 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

359445 (2010 MH96)          Discovered 2010-Jun-28 by WISE at WISE
Reference: 20130327/Numbers.arcLast Updated: 2013-03-29

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