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26536 (2000 DL3)
Classification: Main-belt Asteroid          SPK-ID: 2026536
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 31 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .0797154583700813 3.2903e-08  
a 3.065505884742389 1.6592e-08 au
q 2.821137678003967 1.0446e-07 au
i 8.854419218780079 4.3388e-06 deg
node 175.157307194167 2.4875e-05 deg
peri 289.7607784757036 3.8314e-05 deg
M 264.8322200940325 2.8795e-05 deg
tp 2459118.749743077796
(2020-Sep-26.24974308)
0.00015777 TDB
period 1960.431436903864
5.37
1.5916e-05
4.358e-08
d
yr
n .183633047921611 1.4909e-09 deg/d
Q 3.309874091480809 1.7915e-08 au
  Orbit Determination Parameters
   # obs. used (total)      1620  
   data-arc span      8958 days (24.53 yr)  
   first obs. used      1995-04-23  
   last obs. used      2019-11-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .50658  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-07 04:53:50  

Additional Information
 Earth MOID = 1.85357 au 
 Jupiter MOID = 1.81574 au 
 T_jup = 3.209 
[ 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 13.2   n/a MPO358877  
diameter diameter 8.718 km 0.207 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.161   0.035 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

26536 (2000 DL3)          Discovered 2000-Feb-27 by Korlevic, K., Juric, M. at Visnjan
Reference: 20010705/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 2000 DL3 = 1998 XT84 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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