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15153 (2000 FD17)
Classification: Main-belt Asteroid          SPK-ID: 2015153
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 34 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1494038656343659 4.255e-08  
a 3.104752269684524 1.5903e-08 au
q 2.640890278756584 1.3139e-07 au
i 10.42841766960393 4.0217e-06 deg
node 147.4005410714985 2.2704e-05 deg
peri 228.1594282827535 2.5817e-05 deg
M 49.01222465144021 1.1463e-05 deg
tp 2458728.454985499407
(2019-Sep-01.95498550)
6.395e-05 TDB
period 1998.19954953495
5.47
1.5352e-05
4.203e-08
d
yr
n .1801621865462758 1.3842e-09 deg/d
Q 3.568614260612463 1.8279e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1896  
   data-arc span      14221 days (38.93 yr)  
   first obs. used      1981-11-24  
   last obs. used      2020-10-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .48701  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-13 02:35:27  

Additional Information
 Earth MOID = 1.6543 au 
 Jupiter MOID = 1.93795 au 
 T_jup = 3.178 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456966.5 (2014-Nov-05.0) TDB
Reference: JPL 34 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1472461626455528 4.2433e-08  
q 2.646932194878275 1.3036e-07 au
tp 2456712.812502804189
(2014-Feb-24.31250280)
6.9861e-05 TDB
node 147.6644102081063 2.2548e-05 deg
peri 225.391370432254 2.5927e-05 deg
i 10.46003012550349 4.0332e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      1896  
   data-arc span      14221 days (38.93 yr)  
   first obs. used      1981-11-24  
   last obs. used      2020-10-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .48701  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-13 02:35:27  

Additional Information
 Jupiter MOID = 1.93795 au 
 T_jup = 3.178 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.80056029110036E-15 -5.503747338048015E-15 -1.527510829171793E-13 -1.660358282723049E-15 -6.196950545822591E-14 -2.213204718054759E-15
q -5.503747338048015E-15 1.699308388705648E-14 1.92329914968273E-13 6.521691549201239E-15 1.427312594438456E-13 7.816047022206209E-15
tp -1.527510829171793E-13 1.92329914968273E-13 4.880595325442624E-9 -1.006305606509719E-11 9.187437070086412E-10 -3.165911444555594E-12
node -1.660358282723049E-15 6.521691549201239E-15 -1.006305606509719E-11 5.084334045276768E-10 -5.013311812652589E-10 2.211735427411226E-11
peri -6.196950545822591E-14 1.427312594438456E-13 9.187437070086412E-10 -5.013311812652589E-10 6.721937624308576E-10 -2.227797247493636E-11
i -2.213204718054759E-15 7.816047022206209E-15 -3.165911444555594E-12 2.211735427411226E-11 -2.227797247493636E-11 1.626693524388256E-11

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 12.8   n/a MPO502285  
diameter diameter 20.225 km 0.077 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
rotation period rot_per 9.125 h n/a LCDB (Rev. 2019-August); Warner et al., 2009 Result based on less than full coverage, so that the period may be wrong by 30 percent or so.
Published Reference List:
[Waszczak, A.; Chang, C.-K.; Ofeck, E.O.; Laher, F.; et al. (2015) Astron. J. 150, A75.]
geometric albedo albedo 0.046   0.001 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

15153 (2000 FD17)          Discovered 2000-Mar-28 by LINEAR at Socorro
Reference: 20000523/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 2000 FD17 = 1981 WH1 = 1983 CF4 = 1987 YA2 = 1994 CE6 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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