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266032 (2006 GT39)
Classification: Main-belt Asteroid          SPK-ID: 2266032
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 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .09903416118134854 6.8273e-08  
a 3.175875609618832 6.3629e-08 au
q 2.861355432603927 2.529e-07 au
i 18.29001945090181 6.2047e-06 deg
node 58.73936081704125 1.8117e-05 deg
peri 102.3242500829423 5.2032e-05 deg
M 204.4804197772275 3.9626e-05 deg
tp 2459893.550930634261
(2022-Nov-10.05093063)
0.00022143 TDB
period 2067.253104514602
5.66
6.2126e-05
1.701e-07
d
yr
n .1741441332044966 5.2335e-09 deg/d
Q 3.490395786633737 6.993e-08 au
  Orbit Determination Parameters
   # obs. used (total)      426  
   data-arc span      5345 days (14.63 yr)  
   first obs. used      2003-10-27  
   last obs. used      2018-06-15  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .53875  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Oct-04 10:14:36  

Additional Information
 Earth MOID = 1.9338 au 
 Jupiter MOID = 1.6881 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 14.8   n/a MPO360372  
diameter diameter 7.263 km 0.283 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.048   0.006 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

266032 (2006 GT39)          Discovered 2006-Apr-02 by CSS at Catalina
Reference: 20110218/Numbers.arcLast Updated: 2011-02-22

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