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26579 (2000 EU96)
Classification: Main-belt Asteroid          SPK-ID: 2026579
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 37 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1370209096158835 3.6427e-08  
a 3.147090275325884 2.0409e-08 au
q 2.71587310315743 1.1604e-07 au
i 18.61129819007001 4.0313e-06 deg
node 358.6486139889933 1.2331e-05 deg
peri 232.6521493439857 1.9971e-05 deg
M 233.8671252899547 1.8146e-05 deg
tp 2459914.976619399439
(2022-Dec-01.47661940)
0.00010631 TDB
period 2039.211296619355
5.58
1.9836e-05
5.431e-08
d
yr
n .1765388415593887 1.7173e-09 deg/d
Q 3.578307447494337 2.3205e-08 au
  Orbit Determination Parameters
   # obs. used (total)      2560  
   data-arc span      24020 days (65.76 yr)  
   first obs. used      1955-04-16  
   last obs. used      2021-01-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .40728  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Feb-24 03:20:25  

Additional Information
 Earth MOID = 1.74962 au 
 Jupiter MOID = 1.55164 au 
 T_jup = 3.114 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457593.5 (2016-Jul-24.0) TDB
Reference: JPL 37 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1390299048120252 3.6245e-08  
q 2.709789075472055 1.1596e-07 au
tp 2457876.593104529563
(2017-May-03.09310453)
9.6311e-05 TDB
node 358.6836478328491 1.2317e-05 deg
peri 232.6237226999749 1.9843e-05 deg
i 18.62538279613365 4.0336e-06 deg
  Orbit Determination Parameters
   # obs. used (total)      2560  
   data-arc span      24020 days (65.76 yr)  
   first obs. used      1955-04-16  
   last obs. used      2021-01-19  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .40728  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Feb-24 03:20:25  

Additional Information
 Jupiter MOID = 1.55164 au 
 T_jup = 3.114 
Orbit Covariance (6×6)
  e q tp node peri i
e 1.31369561591329E-15 -4.154343248134805E-15 -3.764989044086504E-13 2.329902842399104E-15 -4.223757364701502E-14 1.492440764534142E-15
q -4.154343248134805E-15 1.344743009186127E-14 1.826542901693266E-12 -6.990259832365796E-15 2.293840570276141E-13 -3.653435201353702E-15
tp -3.764989044086504E-13 1.826542901693266E-12 9.275864855910223E-9 2.27928447691833E-12 1.520168152867501E-9 9.648950075062506E-12
node 2.329902842399104E-15 -6.990259832365796E-15 2.27928447691833E-12 1.517180460054879E-10 -1.431926908387871E-10 2.077677719995069E-12
peri -4.223757364701502E-14 2.293840570276141E-13 1.520168152867501E-9 -1.431926908387871E-10 3.93736215261482E-10 -3.7006029237551E-13
i 1.492440764534142E-15 -3.653435201353702E-15 9.648950075062506E-12 2.077677719995069E-12 -3.7006029237551E-13 1.626973000523541E-11

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 12.51   n/a E2021B10  
diameter diameter 9.794 km 0.331 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
rotation period rot_per 5.95256 h n/a LCDB (Rev. 2020-October); Warner et al., 2009 Result based on less than full coverage, so that the period may be wrong by 30 percent or so.
Published Reference List:
[Pal, A.; Szakats, R.; Kiss, C.; Bodi, A.; et al. (2019) Ap. J. Supl. Ser. 247, id.26.]
geometric albedo albedo 0.202   0.044 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

26579 (2000 EU96)          Discovered 2000-Mar-10 by LINEAR at Socorro
Reference: 20010705/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 2000 EU96 = 1996 TG53 = 1998 YG30 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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