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17223 (2000 CX56)
Classification: Main-belt Asteroid          SPK-ID: 2017223
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 43 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1181321245354304 2.1616e-08  
a 2.567142833724982 9.5315e-09 au
q 2.263880796791145 5.6841e-08 au
i 15.36748867414752 3.9704e-07 deg
node 150.7423877657004 2.3628e-06 deg
peri 225.8045606350503 6.3583e-06 deg
M 72.04844404281728 4.6629e-06 deg
tp 2458899.826202994180
(2020-Feb-20.32620299)
1.9197e-05 TDB
period 1502.358147495429
4.11
8.3672e-06
2.291e-08
d
yr
n .2396232886280502 1.3345e-09 deg/d
Q 2.870404870658819 1.0658e-08 au
  Orbit Determination Parameters
   # obs. used (total)      2599  
   data-arc span      23745 days (65.01 yr)  
   first obs. used      1956-03-10  
   last obs. used      2021-03-14  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      0  
   norm. resid. RMS      .43046  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-13 01:57:40  

Additional Information
 Earth MOID = 1.28412 au 
 Jupiter MOID = 2.62021 au 
 T_jup = 3.372 
[ 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 13.3   n/a MPO502301  
diameter diameter 5.917 km 0.130 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.265   0.017 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

17223 (2000 CX56)          Discovered 2000-Feb-05 by LINEAR at Socorro
Reference: 20000913/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 2000 CX56 = 1993 FW1 = 1998 ML10 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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