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27911 (1996 TC14)
Classification: Main-belt Asteroid          SPK-ID: 2027911
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1065690978357276 4.6761e-08  
a 2.997115894236054 1.7567e-08 au
q 2.677715957278197 1.3772e-07 au
i 8.973987391383721 4.3506e-06 deg
node 266.0016435140863 3.1208e-05 deg
peri 127.0954312024256 3.7748e-05 deg
M 92.83281898928068 2.0116e-05 deg
tp 2458111.788262266724
(2017-Dec-24.28826227)		 0.00010581 TDB
period 1895.194258878365
5.19		 1.6663e-05
4.562e-08		 d
yr
n .1899541423331766 1.6701e-09 deg/d
Q 3.31651583119391 1.9439e-08 au
   Orbit Determination Parameters
   # obs. used (total)      2005  
   data-arc span      23207 days (63.54 yr)  
   first obs. used      1955-10-24  
   last obs. used      2019-05-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .41679  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-May-30 03:29:10  

Additional Information
 Earth MOID = 1.69594 au 
 Jupiter MOID = 2.09865 au 
 T_jup = 3.227 
[ 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 12.3   n/a MPO337494  
diameter diameter 12.226 km 0.223 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.157   0.020 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

27911 (1996 TC14)          Discovered 1996-Oct-10 by Beijing Schmidt CCD Asteroid Program at Xinglong
Reference: 20010902/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1996 TC14 = 1986 VF4 = 2000 LC2 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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