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59694 (1999 JF116)
Classification: Main-belt Asteroid          SPK-ID: 2059694
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 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2387591163400018 3.1895e-08  
a 2.407047324418544 1.021e-08 au
q 1.832342832251806 7.737e-08 au
i 6.453492678436175 4.5426e-06 deg
node 84.82714300509107 2.9312e-05 deg
peri 259.2420125225271 3.0737e-05 deg
M 149.1897163840893 9.9444e-06 deg
tp 2458435.222423921249
(2018-Nov-12.72242392)
3.7e-05 TDB
period 1364.034548228775
3.73
8.6789e-06
2.376e-08
d
yr
n .2639229339663477 1.6792e-09 deg/d
Q 2.981751816585281 1.2648e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1020  
   data-arc span      9053 days (24.79 yr)  
   first obs. used      1995-04-22  
   last obs. used      2020-02-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .55728  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 12:52:30  

Additional Information
 Earth MOID = .838018 au 
 Jupiter MOID = 2.45591 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 15.1   n/a MPO449383  
diameter diameter 2.106 km 0.408 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.302   0.073 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

59694 (1999 JF116)          Discovered 1999-May-13 by LINEAR at Socorro
Reference: 20030614/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1999 JF116 = 2000 WA100 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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