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20759 (2000 CX96)
Classification: Main-belt Asteroid          SPK-ID: 2020759
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]

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Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 33 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1788828865575233 3.0572e-08  
a 2.715004963346377 1.1445e-08 au
q 2.229337038484974 8.1508e-08 au
i 13.47210734440519 3.978e-06 deg
node 172.3899872344929 1.457e-05 deg
peri 130.6060469847399 1.8386e-05 deg
M 50.64919872428376 1.1472e-05 deg
tp 2458770.607688465103
(2019-Oct-14.10768847)		 5.1495e-05 TDB
period 1634.008715578816
4.47		 1.0332e-05
2.829e-08		 d
yr
n .2203170623067803 1.3931e-09 deg/d
Q 3.20067288820778 1.3492e-08 au
   Orbit Determination Parameters
   # obs. used (total)      1960  
   data-arc span      24459 days (66.97 yr)  
   first obs. used      1953-11-11  
   last obs. used      2020-10-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .44802  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-13 02:00:50  

Additional Information
 Earth MOID = 1.24043 au 
 Jupiter MOID = 2.21656 au 
 T_jup = 3.299 
[ 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 13.5   n/a MPO435892  
diameter diameter 5.059 km 0.145 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.229   0.022 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

20759 (2000 CX96)          Discovered 2000-Feb-06 by LINEAR at Socorro
Reference: 20010109/Numbers.arcLast Updated: 2004-04-19

[ show close-approach data ]
Alternate Designations
 2000 CX96 = 1997 TO26 
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances | Close-Approach Data ]
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