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26595 (2000 EJ153)
Classification: Main-belt Asteroid          SPK-ID: 2026595
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 26 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .04846090958995837 5.2564e-08  
a 3.067687555772831 2.104e-08 au
q 2.919024626482284 1.6685e-07 au
i 8.411926865566672 4.7494e-06 deg
node 296.6337957585151 3.3807e-05 deg
peri 267.8072023075307 6.1274e-05 deg
M 287.1508533210659 5.3567e-05 deg
tp 2459597.634010904267
(2022-Jan-18.13401090)		 0.0002933 TDB
period 1962.524620303871
5.37		 2.019e-05
5.528e-08		 d
yr
n .183437189157025 1.8872e-09 deg/d
Q 3.216350485063379 2.206e-08 au
   Orbit Determination Parameters
   # obs. used (total)      1063  
   data-arc span      25551 days (69.95 yr)  
   first obs. used      1951-02-04  
   last obs. used      2021-01-18  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .51836  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Feb-24 03:20:32  

Additional Information
 Earth MOID = 1.93007 au 
 Jupiter MOID = 1.85999 au 
 T_jup = 3.214 
[ 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 14.15   n/a E2021B10  
diameter diameter 4.980 km 0.338 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.236   0.039 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

26595 (2000 EJ153)          Discovered 2000-Mar-06 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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