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14380 (1989 UC6)
Classification: Main-belt Asteroid          SPK-ID: 2014380
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 37 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .241174579607272 1.9638e-08  
a 2.638867889857848 1.1455e-08 au
q 2.002440035882253 5.242e-08 au
i 28.50505397555315 6.595e-07 deg
node 37.541730311946 1.706e-06 deg
peri 254.7687795068663 4.6294e-06 deg
M 164.6022507588785 5.0123e-06 deg
tp 2458484.590429192131
(2019-Jan-01.09042919)
1.8269e-05 TDB
period 1565.758938912512
4.29
1.0195e-05
2.791e-08
d
yr
n .2299204501109447 1.4971e-09 deg/d
Q 3.275295743833444 1.4218e-08 au
  Orbit Determination Parameters
   # obs. used (total)      2103  
   data-arc span      23884 days (65.39 yr)  
   first obs. used      1955-10-24  
   last obs. used      2021-03-15  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .43401  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 00:26:47  

Additional Information
 Earth MOID = 1.14991 au 
 Jupiter MOID = 2.2332 au 
 T_jup = 3.186 
[ 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 13.38   n/a E2021B10  
diameter diameter 17.541 km 0.054 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.028   0.004 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

14380 (1989 UC6)          Discovered 1989-Oct-30 by Bus, S. J. at Cerro Tololo
Reference: 20000418/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1989 UC6 = 2000 DJ 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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