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14276 (2000 CF2)
Classification: Main-belt Asteroid          SPK-ID: 2014276
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 40 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1781627753117972 1.5543e-08  
a 2.250150770301281 6.2436e-09 au
q 1.849257664194426 3.5134e-08 au
i 6.451699736493977 3.4124e-07 deg
node 31.24853791755419 5.7209e-06 deg
peri 343.4307177994121 6.4148e-06 deg
M 186.8644411061926 4.3703e-06 deg
tp 2459793.424816022995
(2022-Aug-01.92481602)
1.6227e-05 TDB
period 1232.865941185423
3.38
5.1314e-06
1.405e-08
d
yr
n .2920025511077494 1.2154e-09 deg/d
Q 2.651043876408135 7.356e-09 au
  Orbit Determination Parameters
   # obs. used (total)      2461  
   data-arc span      15501 days (42.44 yr)  
   first obs. used      1978-09-28  
   last obs. used      2021-03-07  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .43032  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 00:23:37  

Additional Information
 Earth MOID = .850217 au 
 Jupiter MOID = 2.81284 au 
 T_jup = 3.598 
[ 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 13.32   n/a E2021B10  
diameter diameter 5.952 km 0.100 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.345   0.037 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

14276 (2000 CF2)          Discovered 2000-Feb-02 by Kobayashi, T. at Oizumi
Reference: 20000320/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 CF2 = 1978 SN6 = 1983 AK6 = 1983 BO = 1988 SA4 = 1997 GQ12 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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