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441966 (2010 MN37)
Classification: Main-belt Asteroid          SPK-ID: 2441966
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 9 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2144079152292768 9.1178e-08  
a 3.056982534290269 5.8759e-08 au
q 2.401541282220781 2.9314e-07 au
i 26.07803333526063 7.3598e-06 deg
node 174.2672813089497 2.4258e-05 deg
peri 272.381532653327 2.8894e-05 deg
M 155.2219094851415 1.8282e-05 deg
tp 2457758.739807177322
(2017-Jan-05.23980718)
8.8951e-05 TDB
period 1952.260930311335
5.34
5.6288e-05
1.541e-07
d
yr
n .1844015799376723 5.3167e-09 deg/d
Q 3.712423786359757 7.1358e-08 au
  Orbit Determination Parameters
   # obs. used (total)      100  
   data-arc span      5015 days (13.73 yr)  
   first obs. used      2005-10-31  
   last obs. used      2019-07-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .47601  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Sep-24 07:42:36  

Additional Information
 Earth MOID = 1.57751 au 
 Jupiter MOID = 1.9454 au 
 T_jup = 3.047 
[ 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 16.0   n/a MPO440829  
diameter diameter 4.208 km 0.729 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.048   0.022 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

441966 (2010 MN37)          Discovered 2010-Jun-21 by WISE at WISE
Reference: Last Updated: 2015-09-02

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