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186352 (2002 FJ15)
Classification: Main-belt Asteroid          SPK-ID: 2186352
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 17 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1286285314825234 4.2377e-08  
a 3.150014788334288 3.24e-08 au
q 2.744833011962617 1.2891e-07 au
i 8.534573264827019 5.373e-06 deg
node 95.03043887695139 3.9611e-05 deg
peri 137.6944420104029 4.7627e-05 deg
M 79.90031537868576 2.5334e-05 deg
tp 2458747.275572916629
(2019-Sep-20.77557292)
0.00014462 TDB
period 2042.054439669187
5.59
3.1506e-05
8.626e-08
d
yr
n .1762930473383071 2.72e-09 deg/d
Q 3.555196564705959 3.6568e-08 au
  Orbit Determination Parameters
   # obs. used (total)      457  
   data-arc span      7195 days (19.70 yr)  
   first obs. used      2000-12-03  
   last obs. used      2020-08-15  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .57451  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 21:50:55  

Additional Information
 Earth MOID = 1.73933 au 
 Jupiter MOID = 1.49236 au 
 T_jup = 3.178 
[ show covariance matrix ]

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 15.00   n/a E2021B55  
diameter diameter 6.514 km 0.238 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.046   0.004 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

186352 (2002 FJ15)          Discovered 2002-Mar-16 by NEAT at Haleakala
Reference: 20080520/Numbers.arcLast Updated: 2008-05-22

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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