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392419 (2010 MT80)
Classification: Outer Main-belt Asteroid          SPK-ID: 2392419
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09452886848536995 6.7262e-08  
a 3.233760367930471 9.4381e-08 au
q 2.92807665939717 2.4077e-07 au
i 16.31745701443999 1.325e-05 deg
node 337.0168312359254 3.3432e-05 deg
peri 293.0008156476831 0.00010656 deg
M 321.7187705040263 0.0001132 deg
tp 2459226.362200535986
(2021-Jan-11.86220054)
0.00067309 TDB
period 2124.027709232981
5.82
9.2988e-05
2.546e-07
d
yr
n .1694893143037204 7.4201e-09 deg/d
Q 3.539444076463772 1.033e-07 au
  Orbit Determination Parameters
   # obs. used (total)      118  
   data-arc span      5286 days (14.47 yr)  
   first obs. used      2004-09-18  
   last obs. used      2019-03-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52092  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-14 13:38:32  

Additional Information
 Earth MOID = 1.95841 au 
 Jupiter MOID = 1.83297 au 
 T_jup = 3.115 
[ 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 15.4   n/a MPO254799  
diameter diameter 6.096 km 2.405 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.033   0.016 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

392419 (2010 MT80)          Discovered 2010-Jun-26 by WISE at WISE
Reference: Last Updated: 2014-04-17

[ show close-approach data ]
Alternate Designations
 2010 MT80 = 2004 SC42 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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