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24485 (2000 YL102)
Classification: Jupiter Trojan          SPK-ID: 2024485
[ 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 32 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .04268099620665832 5.1804e-08  
a 5.142681178104088 8.4649e-08 au
q 4.923186422249374 2.7231e-07 au
i 13.2743919420172 5.8449e-06 deg
node 151.2515009889096 1.68e-05 deg
peri 190.3687419355839 5.6708e-05 deg
M 14.47732358505958 5.1678e-05 deg
tp 2458829.195564125973
(2019-Dec-11.69556413)		 0.00061394 TDB
period 4259.737412949178
11.66		 0.00010517
2.879e-07		 d
yr
n .08451225160162121 2.0866e-09 deg/d
Q 5.362175933958802 8.8262e-08 au
   Orbit Determination Parameters
   # obs. used (total)      1497  
   data-arc span      13968 days (38.24 yr)  
   first obs. used      1982-08-12  
   last obs. used      2020-11-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .48507  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Dec-18 03:25:55  

Additional Information
 Earth MOID = 3.915 au 
 Jupiter MOID = .0458709 au 
 T_jup = 2.945 
[ 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 11.4   n/a MPO365542  
diameter diameter 26.422 km 0.322 urn:nasa:pds:neowise_diameters_albedos::2.0[jupiter_trojans] (http://adsabs.harvard.edu/abs/2012ApJ...759...49G)  
geometric albedo albedo 0.084   0.012 urn:nasa:pds:neowise_diameters_albedos::2.0[jupiter_trojans] (http://adsabs.harvard.edu/abs/2012ApJ...759...49G)  

24485 (2000 YL102)          Discovered 2000-Dec-28 by LINEAR at Socorro
Reference: 20010408/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 YL102 = 1996 RR28 = 2000 AK174 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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