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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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 29 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1067749040839367 4.6251e-08  
a 2.996026815214476 1.657e-08 au
q 2.676126339387047 1.3633e-07 au
i 8.973982849802937 4.086e-06 deg
node 266.0009475536693 3.0974e-05 deg
peri 126.9062203922522 3.6579e-05 deg
M 169.0390984599593 1.9109e-05 deg
tp 2458111.090757802032
(2017-Dec-23.59075780)		 9.9598e-05 TDB
period 1894.161351476399
5.19		 1.5714e-05
4.302e-08		 d
yr
n .1900577264547178 1.5767e-09 deg/d
Q 3.315927291041904 1.834e-08 au
   Orbit Determination Parameters
   # obs. used (total)      2116  
   data-arc span      23478 days (64.28 yr)  
   first obs. used      1955-10-24  
   last obs. used      2020-02-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .42299  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 01:12:42  

Additional Information
 Earth MOID = 1.69497 au 
 Jupiter MOID = 2.10075 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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