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14248 (2000 AF56)
Classification: Main-belt Asteroid          SPK-ID: 2014248
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 37 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1784153173851585 2.9555e-08  
a 3.161991060755362 1.2706e-08 au
q 2.59784342208166 9.3992e-08 au
i 1.413485815900696 3.4066e-06 deg
node 146.5242115510748 0.0001167 deg
peri 206.4042804182787 0.00011706 deg
M 49.4716419200768 7.8255e-06 deg
tp 2459114.276478037784
(2020-Sep-21.77647804)
4.4747e-05 TDB
period 2053.711256855737
5.62
1.2379e-05
3.389e-08
d
yr
n .1752924121140405 1.0566e-09 deg/d
Q 3.726138699429063 1.4973e-08 au
  Orbit Determination Parameters
   # obs. used (total)      2247  
   data-arc span      14376 days (39.36 yr)  
   first obs. used      1981-10-04  
   last obs. used      2021-02-12  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .48147  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Jul-08 17:14:49  

Additional Information
 Earth MOID = 1.59186 au 
 Jupiter MOID = 1.71337 au 
 T_jup = 3.179 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 13.40   n/a E2021B10  
diameter diameter 11.199 km 0.162 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.070   0.010 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

14248 (2000 AF56)          Discovered 2000-Jan-04 by LINEAR at Socorro
Reference: 20000320/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 2000 AF56 = 1981 TC = 1981 TT3 = 1991 KS2 = 1991 LO6 = 1996 FO19 = 1998 VN23 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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