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67343 (2000 JL24)
Classification: Main-belt Asteroid          SPK-ID: 2067343
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 30 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2086042236677167 3.5723e-08  
a 2.381061911583491 7.9614e-09 au
q 1.884362340012847 8.7485e-08 au
i 13.1036105530676 3.5338e-06 deg
node 248.9728034209311 1.7414e-05 deg
peri 99.93107695334898 1.9993e-05 deg
M 165.5255387616603 9.0702e-06 deg
tp 2458779.454814433492
(2019-Oct-22.95481443)
3.2899e-05 TDB
period 1342.006003821539
3.67
6.7307e-06
1.843e-08
d
yr
n .2682551337138973 1.3454e-09 deg/d
Q 2.877761483154134 9.6222e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1507  
   data-arc span      24657 days (67.51 yr)  
   first obs. used      1953-10-08  
   last obs. used      2021-04-11  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .43759  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Jul-08 22:35:27  

Additional Information
 Earth MOID = .930557 au 
 Jupiter MOID = 2.70713 au 
 T_jup = 3.474 
[ 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 14.56   n/a MPCxxxxx  
diameter diameter 3.930 km 1.041 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.181   0.070 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

67343 (2000 JL24)          Discovered 2000-May-07 by LINEAR at Socorro
Reference: 20030910/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 JL24 = 2001 TP1 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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