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52519 (1996 JL1)
Classification: Main-belt Asteroid          SPK-ID: 2052519
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 28 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .04856267430473513 4.1013e-08  
a 2.610738036877867 1.4627e-08 au
q 2.483953615897984 1.1128e-07 au
i 14.40527151100209 5.0396e-06 deg
node 56.27937616139302 1.8113e-05 deg
peri 234.9387655851271 6.0514e-05 deg
M 243.1668845941193 5.9329e-05 deg
tp 2459700.542397225558
(2022-May-01.04239723)
0.00025402 TDB
period 1540.789718529922
4.22
1.2949e-05
3.545e-08
d
yr
n .2336464188919163 1.9636e-09 deg/d
Q 2.737522457857751 1.5338e-08 au
  Orbit Determination Parameters
   # obs. used (total)      904  
   data-arc span      9079 days (24.86 yr)  
   first obs. used      1996-05-15  
   last obs. used      2021-03-24  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .55385  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-May-04 06:18:41  

Additional Information
 Earth MOID = 1.49029 au 
 Jupiter MOID = 2.33299 au 
 T_jup = 3.364 
[ 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 14.8   n/a MPO319707  
diameter diameter 3.088 km 0.760 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.294   0.112 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

52519 (1996 JL1)          Discovered 1996-May-15 by NEAT at Haleakala
Reference: 20030216/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1996 JL1 = 2000 GP141 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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