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JPL Small-Body Database Browser
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23152 (2000 CS8)
Classification: Jupiter Trojan          SPK-ID: 2023152
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]

[ show orbit diagram ]
Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 22 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1504078850486196 7.3075e-08  
a 5.216925817908232 1.4957e-07 au
q 4.432259039181115 4.437e-07 au
i 11.42885010494454 6.2745e-06 deg
node 129.3302041630833 3.8258e-05 deg
peri 293.078890526146 4.591e-05 deg
M 264.6182882531286 3.141e-05 deg
tp 2459753.642636755113
(2022-Jun-23.14263676)
0.00040804 TDB
period 4352.315990444127
11.92
0.00018717
5.124e-07
d
yr
n .0827145824867519 3.5571e-09 deg/d
Q 6.001592596635349 1.7206e-07 au
  Orbit Determination Parameters
   # obs. used (total)      649  
   data-arc span      23976 days (65.64 yr)  
   first obs. used      1954-02-10  
   last obs. used      2019-10-03  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .56574  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-07 04:36:00  

Additional Information
 Earth MOID = 3.46641 au 
 Jupiter MOID = .246144 au 
 T_jup = 2.938 
[ 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 11.9   n/a MPO492990  
diameter diameter 19.483 km 0.725 urn:nasa:pds:neowise_diameters_albedos::2.0[jupiter_trojans] (http://adsabs.harvard.edu/abs/2012ApJ...759...49G)  
geometric albedo albedo 0.097   0.009 urn:nasa:pds:neowise_diameters_albedos::2.0[jupiter_trojans] (http://adsabs.harvard.edu/abs/2012ApJ...759...49G)  

23152 (2000 CS8)          Discovered 2000-Feb-02 by LINEAR at Socorro
Reference: 20010309/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 2000 CS8 = 1977 CT1 = 1996 RV29 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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