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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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1324713592912226 3.8999e-08  
a 2.358211355301953 7.2478e-09 au
q 2.045815891569107 9.4127e-08 au
i 7.731667858905687 4.1411e-06 deg
node 156.407312816227 2.4581e-05 deg
peri 183.0797399130325 2.8053e-05 deg
M 309.5228960707825 1.2628e-05 deg
tp 2458785.966059676863
(2019-Oct-29.46605968)		 4.6379e-05 TDB
period 1322.733997919077
3.62		 6.098e-06
1.67e-08		 d
yr
n .2721635646822048 1.2547e-09 deg/d
Q 2.670606819034798 8.2079e-09 au
   Orbit Determination Parameters
   # obs. used (total)      1488  
   data-arc span      17753 days (48.61 yr)  
   first obs. used      1971-03-25  
   last obs. used      2019-11-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .52091  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-07 04:54:20  

Additional Information
 Earth MOID = 1.03602 au 
 Jupiter MOID = 2.70111 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 14.5   n/a MPO337483  
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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