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26583 (2000 EF109)
Classification: Main-belt Asteroid          SPK-ID: 2026583
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 24 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .06472620541749212 3.9326e-08  
a 3.151136722832192 2.4459e-08 au
q 2.947175600011553 1.2889e-07 au
i 12.84343970744257 4.4059e-06 deg
node 246.1971663010505 2.1631e-05 deg
peri 190.8514425707777 4.7552e-05 deg
M 223.9346980246985 4.4314e-05 deg
tp 2459372.725584983606
(2021-Jun-07.22558498)
0.00025495 TDB
period 2043.145508504151
5.59
2.3789e-05
6.513e-08
d
yr
n .1761989043372476 2.0515e-09 deg/d
Q 3.355097845652831 2.6043e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1110  
   data-arc span      9896 days (27.09 yr)  
   first obs. used      1992-09-24  
   last obs. used      2019-10-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .5602  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-07 04:54:19  

Additional Information
 Earth MOID = 1.96281 au 
 Jupiter MOID = 1.93657 au 
 T_jup = 3.166 
[ 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 13.5   n/a MPO358878  
diameter diameter 8.524 km 0.080 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.116   0.023 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

26583 (2000 EF109)          Discovered 2000-Mar-08 by JPL/GEODSS NEAT at Haleakala
Reference: 20010705/Numbers.arcLast Updated: 2004-04-19

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