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15082 (1999 CT30)
Classification: Main-belt Asteroid          SPK-ID: 2015082
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 41 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .007451414222717568 3.4334e-08  
a 3.153702092735839 1.7566e-08 au
q 3.130202552107813 1.1346e-07 au
i 9.061183817994131 4.2482e-06 deg
node 339.2804984710815 2.1509e-05 deg
peri 123.3190146364989 0.0003012 deg
M 3.986445209570328 0.00029842 deg
tp 2459177.847678075616
(2020-Nov-24.34767808)
0.0016958 TDB
period 2045.641032065548
5.60
1.7091e-05
4.679e-08
d
yr
n .1759839553259727 1.4703e-09 deg/d
Q 3.177201633363866 1.7697e-08 au
  Orbit Determination Parameters
   # obs. used (total)      2698  
   data-arc span      15185 days (41.57 yr)  
   first obs. used      1979-08-23  
   last obs. used      2021-03-20  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .43133  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-May-04 01:56:57  

Additional Information
 Earth MOID = 2.14933 au 
 Jupiter MOID = 1.82014 au 
 T_jup = 3.187 
[ 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 12.42   n/a MPCxxxxx  
diameter diameter 18.076 km 0.147 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2014ApJ...791..121M)  
geometric albedo albedo 0.054   0.007 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2012ApJ...759L...8M)  

15082 (1999 CT30)          Discovered 1999-Feb-10 by LINEAR at Socorro
Reference: 20000523/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 1999 CT30 = 1979 QJ4 = 1985 SX = 1985 TU2 = 1996 RA8 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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