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393286 (2013 YR6)
Classification: Main-belt Asteroid          SPK-ID: 2393286
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1808151102618251 8.9748e-08  
a 2.638829514934537 3.1765e-08 au
q 2.16168926522949 2.4411e-07 au
i 13.09413921386821 7.2212e-06 deg
node 93.26717168980302 3.3252e-05 deg
peri 288.9803688432165 3.6214e-05 deg
M 278.3961044728931 1.6014e-05 deg
tp 2459555.414560427039
(2021-Dec-06.91456043)
7.1693e-05 TDB
period 1565.724784686192
4.29
2.8271e-05
7.74e-08
d
yr
n .2299254655230819 4.1516e-09 deg/d
Q 3.115969764639583 3.7509e-08 au
  Orbit Determination Parameters
   # obs. used (total)      288  
   data-arc span      5779 days (15.82 yr)  
   first obs. used      2004-09-21  
   last obs. used      2020-07-18  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .57073  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-14 11:33:36  

Additional Information
 Earth MOID = 1.206 au 
 Jupiter MOID = 2.42974 au 
 T_jup = 3.336 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 16.26   n/a E2021B25  
diameter diameter 4.784 km 0.226 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.064   0.011 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

393286 (2013 YR6)          Discovered 2004-Sep-21 by LONEOS at Anderson Mesa
Reference: Last Updated: 2014-04-17

Alternate Designations
 2013 YR6 = 2010 GK96 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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