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JPL Small-Body Database Browser
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26590 (2000 EY136)
Classification: Main-belt Asteroid          SPK-ID: 2026590
[ 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 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .132267039541536 3.8945e-08  
a 2.357652608996355 7.1481e-09 au
q 2.045812878137028 9.3922e-08 au
i 7.732657299221992 4.1285e-06 deg
node 156.3985514192507 2.437e-05 deg
peri 183.1994221221918 2.7869e-05 deg
M 58.32107934699815 1.257e-05 deg
tp 2458786.289280590402
(2019-Oct-29.78928059)		 4.619e-05 TDB
period 1322.263919853611
3.62		 6.0134e-06
1.646e-08		 d
yr
n .2722603215550614 1.2382e-09 deg/d
Q 2.669492339855681 8.0935e-09 au
   Orbit Determination Parameters
   # obs. used (total)      1514  
   data-arc span      17790 days (48.71 yr)  
   first obs. used      1971-03-25  
   last obs. used      2019-12-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52322  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-23 00:47:54  

Additional Information
 Earth MOID = 1.03696 au 
 Jupiter MOID = 2.70536 au 
 T_jup = 3.529 
[ 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 14.6   n/a MPO502356  
diameter diameter 3.312 km 0.703 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.307   0.233 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

26590 (2000 EY136)          Discovered 2000-Mar-12 by LINEAR at Socorro
Reference: 20010705/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 EY136 = 1990 OS5 = 1998 XM80 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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