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86483 (2000 CT111)
Classification: Main-belt Asteroid          SPK-ID: 2086483
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2002164871326172 4.7687e-08  
a 2.326291246673745 1.1751e-08 au
q 1.860529385217371 1.1251e-07 au
i 3.346211661851536 4.4226e-06 deg
node 86.00997029501339 9.6482e-05 deg
peri 320.2400374178229 9.7446e-05 deg
M 337.727929721779 1.8035e-05 deg
tp 2459080.677524693880
(2020-Aug-19.17752469)
6.5342e-05 TDB
period 1295.968831331404
3.55
9.8199e-06
2.689e-08
d
yr
n .2777844584658388 2.1049e-09 deg/d
Q 2.792053108130119 1.4104e-08 au
  Orbit Determination Parameters
   # obs. used (total)      617  
   data-arc span      7242 days (19.83 yr)  
   first obs. used      1998-06-22  
   last obs. used      2018-04-20  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5413  
   source      ORB  
   producer      Otto Matic  
   solution date      2018-Oct-04 03:09:30  

Additional Information
 Earth MOID = .871721 au 
 Jupiter MOID = 2.59723 au 
 T_jup = 3.545 
[ 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 16.1   n/a MPO436380  
diameter diameter 1.428 km 0.130 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.315   0.100 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

86483 (2000 CT111)          Discovered 2000-Feb-06 by CSS at Catalina
Reference: 20040830/Numbers.arcLast Updated: 2004-09-06

Alternate Designations
 2000 CT111 = 1998 MA18 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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