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15297 (1992 CF)
Classification: Main-belt Asteroid          SPK-ID: 2015297
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 41 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .05356810437415806 2.2141e-08  
a 2.380223630746173 8.666e-09 au
q 2.252719562860525 5.1797e-08 au
i 9.700688461026093 1.0106e-06 deg
node 283.9741015017448 5.5279e-06 deg
peri 307.5662489027449 2.1582e-05 deg
M 278.1594475357156 1.9483e-05 deg
tp 2459701.423658843464
(2022-May-01.92365884)
7.3077e-05 TDB
period 1341.297362717001
3.67
7.3251e-06
2.006e-08
d
yr
n .2683968596424923 1.4658e-09 deg/d
Q 2.507727698631822 9.1302e-09 au
  Orbit Determination Parameters
   # obs. used (total)      2260  
   data-arc span      24643 days (67.47 yr)  
   first obs. used      1953-11-30  
   last obs. used      2021-05-20  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .45309  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Jul-08 17:26:14  

Additional Information
 Earth MOID = 1.25294 au 
 Jupiter MOID = 2.54589 au 
 T_jup = 3.518 
[ 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 13.48   n/a E2021B10  
diameter diameter 4.780 km 0.122 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.445   0.082 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

15297 (1992 CF)          Discovered 1992-Feb-08 by Otomo, S. at Kiyosato
Reference: 20000621/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1992 CF = 1997 UL21 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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