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26371 (1999 CT64)
Classification: Main-belt Asteroid          SPK-ID: 2026371
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 27 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2013370804547392 4.5141e-08  
a 3.083490867949746 1.7885e-08 au
q 2.462669818987894 1.429e-07 au
i 15.33772313990718 5.2586e-06 deg
node 198.5684437343222 1.4974e-05 deg
peri 188.5407188753856 1.8459e-05 deg
M 350.9840809334158 1.0872e-05 deg
tp 2458650.030182757759
(2019-Jun-15.53018276)
5.9901e-05 TDB
period 1977.709167652112
5.41
1.7206e-05
4.711e-08
d
yr
n .1820287865820955 1.5837e-09 deg/d
Q 3.704311916911598 2.1485e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1345  
   data-arc span      12102 days (33.13 yr)  
   first obs. used      1986-09-12  
   last obs. used      2019-10-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51646  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-07 04:52:46  

Additional Information
 Earth MOID = 1.46703 au 
 Jupiter MOID = 1.74908 au 
 T_jup = 3.142 
[ 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 13.4   n/a MPO452538  
diameter diameter 12.806 km 0.264 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.068   0.011 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

26371 (1999 CT64)          Discovered 1999-Feb-12 by LINEAR at Socorro
Reference: 20010705/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1999 CT64 = 1986 RU15 = 1997 QT3 = 2000 GB30 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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