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243789 (2000 SD67)
Classification: Main-belt Asteroid          SPK-ID: 2243789
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459396.5 (2021-Jul-01.0) TDB
Reference: JPL 21 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2385660672195115 4.5302e-08  
a 2.323926141380828 8.6519e-09 au
q 1.769516221322989 1.0754e-07 au
i 4.373343432041427 4.1576e-06 deg
node 5.436658480741658 5.3533e-05 deg
peri 305.1457891296411 5.4323e-05 deg
M 345.574661728542 8.3911e-06 deg
tp 2459448.350794342710
(2021-Aug-21.85079434)
3.0302e-05 TDB
period 1293.992945753574
3.54
7.2262e-06
1.978e-08
d
yr
n .2782086263927422 1.5536e-09 deg/d
Q 2.878336061438666 1.0716e-08 au
  Orbit Determination Parameters
   # obs. used (total)      379  
   data-arc span      7593 days (20.79 yr)  
   first obs. used      2000-09-20  
   last obs. used      2021-07-05  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .56866  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Jul-09 11:38:35  

Additional Information
 Earth MOID = .759235 au 
 Jupiter MOID = 2.41308 au 
 T_jup = 3.533 
[ 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 17.03   n/a E2021B55  
diameter diameter 2.606 km 0.089 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.041   0.007 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

243789 (2000 SD67)          Discovered 2000-Sep-24 by LINEAR at Socorro
Reference: 20100726/Numbers.arcLast Updated: 2010-07-28

Alternate Designations
 2000 SD67 = 2006 EP3 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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