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100105 (1993 FK35)
Classification: Main-belt Asteroid          SPK-ID: 2100105
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 19 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1094477494135159 5.1525e-08  
a 2.97297026444923 1.993e-08 au
q 2.647585359931956 1.6234e-07 au
i 4.788134656198114 5.1347e-06 deg
node 36.13919395246105 5.2287e-05 deg
peri 284.8493295596917 5.801e-05 deg
M 349.1199123965374 2.2869e-05 deg
tp 2459057.086673781052
(2020-Jul-26.58667378)
0.00011897 TDB
period 1872.338100907877
5.13
1.8828e-05
5.155e-08
d
yr
n .1922729659912596 1.9334e-09 deg/d
Q 3.298355168966503 2.2111e-08 au
  Orbit Determination Parameters
   # obs. used (total)      626  
   data-arc span      9996 days (27.37 yr)  
   first obs. used      1993-03-19  
   last obs. used      2020-07-31  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52234  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-25 09:02:06  

Additional Information
 Earth MOID = 1.64024 au 
 Jupiter MOID = 2.00173 au 
 T_jup = 3.248 
[ 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 MPO436466  
diameter diameter 5.031 km 0.318 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.070   0.010 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

100105 (1993 FK35)          Discovered 1993-Mar-19 by UESAC at La Silla
Reference: 20051019/Numbers.arcLast Updated: 2005-10-26

Alternate Designations
 1993 FK35 = 2000 SF113 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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