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34544 (2000 SP233)
Classification: Main-belt Asteroid          SPK-ID: 2034544
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1077324254435076 3.6853e-08  
a 2.250740920468818 7.6208e-09 au
q 2.008263142061759 8.2414e-08 au
i 7.315185607562821 3.395e-06 deg
node 111.8286013693285 3.11e-05 deg
peri 94.62450332540912 3.4809e-05 deg
M 88.79614629075375 1.5769e-05 deg
tp 2458696.286624887156
(2019-Jul-31.78662489)
5.3797e-05 TDB
period 1233.35099117953
3.38
6.264e-06
1.715e-08
d
yr
n .2918877128851289 1.4825e-09 deg/d
Q 2.493218698875876 8.4418e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1263  
   data-arc span      10387 days (28.44 yr)  
   first obs. used      1992-02-23  
   last obs. used      2020-08-01  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .53754  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-25 03:03:36  

Additional Information
 Earth MOID = 1.01942 au 
 Jupiter MOID = 2.49264 au 
 T_jup = 3.609 
[ 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 15.4   n/a MPO436006  
diameter diameter 2.733 km 0.518 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.164   0.067 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

34544 (2000 SP233)          Discovered 2000-Sep-21 by LINEAR at Socorro
Reference: 20020128/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 SP233 = 1999 GO44 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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