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67581 (2000 SB119)
Classification: Main-belt Asteroid          SPK-ID: 2067581
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 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1772220379937221 3.1967e-08  
a 2.23905179103412 6.6908e-09 au
q 1.842242469453559 7.0852e-08 au
i 4.198164618088386 4.37e-06 deg
node 40.11025520471379 4.5422e-05 deg
peri 271.5752286312745 4.7575e-05 deg
M 120.2505570187953 1.3114e-05 deg
tp 2458987.729795995138
(2020-May-18.22979600)
4.4712e-05 TDB
period 1223.755441055874
3.35
5.4853e-06
1.502e-08
d
yr
n .2941764244082844 1.3186e-09 deg/d
Q 2.63586111261468 7.8765e-09 au
  Orbit Determination Parameters
   # obs. used (total)      950  
   data-arc span      11036 days (30.21 yr)  
   first obs. used      1990-10-25  
   last obs. used      2021-01-11  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .47876  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Jul-08 22:36:04  

Additional Information
 Earth MOID = .83342 au 
 Jupiter MOID = 2.63222 au 
 T_jup = 3.612 
[ 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 16.33   n/a E2021B10  
diameter diameter 1.511 km 0.249 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.162   0.035 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

67581 (2000 SB119)          Discovered 2000-Sep-24 by LINEAR at Socorro
Reference: 20030910/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 SB119 = 2002 CS171 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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