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26589 (2000 EN133)
Classification: Main-belt Asteroid          SPK-ID: 2026589
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 28 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2794179844760561 4.413e-08  
a 2.644584504209816 1.5377e-08 au
q 1.905640032266899 1.1803e-07 au
i 4.847560626897624 4.3357e-06 deg
node 21.40898033345872 5.5475e-05 deg
peri 309.920862543877 5.5785e-05 deg
M 118.4969230620978 7.8187e-06 deg
tp 2458483.442106111481
(2018-Dec-30.94210611)
3.1644e-05 TDB
period 1570.849579801499
4.30
1.3701e-05
3.751e-08
d
yr
n .2291753485686972 1.9988e-09 deg/d
Q 3.383528976152733 1.9674e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1272  
   data-arc span      14603 days (39.98 yr)  
   first obs. used      1980-11-01  
   last obs. used      2020-10-25  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51732  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-13 01:28:03  

Additional Information
 Earth MOID = .899728 au 
 Jupiter MOID = 2.00833 au 
 T_jup = 3.332 
[ 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 14.0   n/a MPO449157  
diameter diameter 3.425 km 0.483 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2015ApJ...814..117N)  
geometric albedo albedo 0.373   0.139 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2015ApJ...814..117N)  

26589 (2000 EN133)          Discovered 2000-Mar-11 by LINEAR at Socorro
Reference: 20010705/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 2000 EN133 = 1980 VQ3 = 1984 SS4 = 1997 RE9 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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