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243787 (2000 SF59)
Classification: Main-belt Asteroid          SPK-ID: 2243787
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 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2456963198653086 4.922e-08  
a 2.372635574032348 1.5021e-08 au
q 1.789687745111086 1.1385e-07 au
i 4.562186712598379 4.7527e-06 deg
node 204.7761498322213 6.5055e-05 deg
peri 149.8757072021862 6.6159e-05 deg
M 143.9704218700776 1.7234e-05 deg
tp 2458466.654286531475
(2018-Dec-14.15428653)
5.997e-05 TDB
period 1334.888474676422
3.65
1.2677e-05
3.471e-08
d
yr
n .2696854507544267 2.5611e-09 deg/d
Q 2.955583402953609 1.8712e-08 au
  Orbit Determination Parameters
   # obs. used (total)      327  
   data-arc span      7090 days (19.41 yr)  
   first obs. used      2000-09-03  
   last obs. used      2020-02-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5559  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-25 09:25:08  

Additional Information
 Earth MOID = .786992 au 
 Jupiter MOID = 2.50224 au 
 T_jup = 3.498 
[ 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 16.5   n/a MPO450093  
diameter diameter 2.923 km 0.391 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.047   0.009 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

243787 (2000 SF59)          Discovered 2000-Sep-24 by LINEAR at Socorro
Reference: 20100726/Numbers.arcLast Updated: 2010-07-28

Alternate Designations
 2000 SF59 = 2006 DV149 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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