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14706 (2000 CQ2)
Classification: Main-belt Asteroid          SPK-ID: 2014706
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 .1766413904010267 3.9162e-08  
a 2.598637659942729 1.3459e-08 au
q 2.139610690541975 1.0482e-07 au
i 13.90025691425634 4.5597e-06 deg
node 28.26964866660509 1.5787e-05 deg
peri 284.3666841325632 2.0214e-05 deg
M 157.8211111131921 1.1456e-05 deg
tp 2458329.720757430649
(2018-Jul-30.22075743)
4.9254e-05 TDB
period 1530.090148407156
4.19
1.1887e-05
3.254e-08
d
yr
n .2352802548103227 1.8278e-09 deg/d
Q 3.057664629343483 1.5836e-08 au
  Orbit Determination Parameters
   # obs. used (total)      3067  
   data-arc span      17740 days (48.57 yr)  
   first obs. used      1971-05-13  
   last obs. used      2019-12-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .37889  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Dec-13 23:49:37  

Additional Information
 Earth MOID = 1.17672 au 
 Jupiter MOID = 2.39194 au 
 T_jup = 3.353 
[ 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 12.8   n/a MPO319268  
diameter diameter 7.134 km 0.052 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2014ApJ...791..121M)  
geometric albedo albedo 0.289   0.039 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2012ApJ...759L...8M)  

14706 (2000 CQ2)          Discovered 2000-Feb-04 by Kobayashi, T. at Oizumi
Reference: 20000418/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 CQ2 = 1985 UX = 1998 XJ69 = 4644 T-1 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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