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344596 (2003 CP24)
Classification: Main-belt Asteroid          SPK-ID: 2344596
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 13 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1750057525332313 7.7003e-08  
a 2.388029744565765 2.119e-08 au
q 1.970110802046293 1.7606e-07 au
i 4.188912190148089 9.2593e-06 deg
node 324.9373675006709 7.2454e-05 deg
peri 226.7039263390478 7.5663e-05 deg
M 105.2571407191325 1.8635e-05 deg
tp 2458206.399403365774
(2018-Mar-28.89940337)
7.0628e-05 TDB
period 1347.901090785877
3.69
1.794e-05
4.912e-08
d
yr
n .2670819116186831 3.5548e-09 deg/d
Q 2.805948687085237 2.4898e-08 au
  Orbit Determination Parameters
   # obs. used (total)      154  
   data-arc span      6096 days (16.69 yr)  
   first obs. used      2003-01-17  
   last obs. used      2019-09-26  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .65302  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Nov-08 10:24:47  

Additional Information
 Earth MOID = .973522 au 
 Jupiter MOID = 2.1684 au 
 T_jup = 3.509 
[ 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 17.5   n/a MPO434167  
diameter diameter 2.018 km 0.239 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.048   0.013 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

344596 (2003 CP24)          Discovered 2003-Feb-03 by NEAT at Palomar
Reference: 20121128/Numbers.arcLast Updated: 2012-12-03

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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