Skip Page Navigation
NASA JPL Caltech
NASA Logo - Jet Propulsion Laboratory + View the NASA Portal
+ Center for Near-Earth Object Studies
JPL Home Earth Solar System Stars & Galaxies Technology
JPL Solar System Dynamics
BODIES ORBITS EPHEMERIDES TOOLS PHYSICAL DATA DISCOVERY FAQ SITE MAP
JPL Small-Body Database Browser
Search: [ help ]  
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 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457339.5 (2015-Nov-13.0) TDB
Reference: JPL 32 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .04142519522496993 5.1677e-08  
q 4.930884951458582 2.6833e-07 au
tp 2458815.043976362884
(2019-Nov-27.54397636)
0.00063721 TDB
node 151.2843179312943 1.68e-05 deg
peri 188.8850719173636 5.8566e-05 deg
i 13.27266812632129 5.8452e-06 deg
  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
 Jupiter MOID = .0458709 au 
 T_jup = 2.945 
Orbit Covariance (6×6)
  e q tp node peri i
e 2.670547182357613E-15 -1.32097731131367E-14 4.07195648573966E-12 2.531167408753456E-15 3.284690390366928E-13 3.906515180138201E-16
q -1.32097731131367E-14 7.200164482209259E-14 -5.123075358185842E-11 -3.437309150301555E-15 -4.515817073217315E-12 2.015944020765126E-15
tp 4.07195648573966E-12 -5.123075358185842E-11 4.060413675628072E-7 -1.603636348649801E-11 3.575173226029446E-8 -6.505675293346859E-12
node 2.531167408753456E-15 -3.437309150301555E-15 -1.603636348649801E-11 2.822244242858986E-10 -2.762110802954139E-10 3.556324661069885E-11
peri 3.284690390366928E-13 -4.515817073217315E-12 3.575173226029446E-8 -2.762110802954139E-10 3.429992220409588E-9 -3.527775521400075E-11
i 3.906515180138201E-16 2.015944020765126E-15 -6.505675293346859E-12 3.556324661069885E-11 -3.527775521400075E-11 3.416664004047425E-11

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 ]
ABOUT SSD CREDITS/AWARDS PRIVACY/COPYRIGHT GLOSSARY LINKS
FirstGov 2021-Jan-25 02:45 UT
(server date/time)  
NASA Home Page
Site Manager:   Ryan S. Park
Webmaster  Alan B. Chamberlin