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80792 (2000 CN86)
Classification: Main-belt Asteroid          SPK-ID: 2080792
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 23 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2153176301167921 4.8946e-08  
a 2.437982142126626 6.9731e-09 au
q 1.913041605016861 1.2111e-07 au
i 11.92119640285164 5.0902e-06 deg
node 344.3109493564999 1.8049e-05 deg
peri 318.2379224587337 2.0015e-05 deg
M 345.8323655413851 7.3569e-06 deg
tp 2459055.219113065618
(2020-Jul-24.71911307)
2.8378e-05 TDB
period 1390.41424037054
3.81
5.9653e-06
1.633e-08
d
yr
n .2589156450987308 1.1108e-09 deg/d
Q 2.962922679236392 8.4746e-09 au
  Orbit Determination Parameters
   # obs. used (total)      1363  
   data-arc span      7987 days (21.87 yr)  
   first obs. used      1998-12-17  
   last obs. used      2020-10-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .49351  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Nov-12 21:17:58  

Additional Information
 Earth MOID = .916038 au 
 Jupiter MOID = 2.36946 au 
 T_jup = 3.442 
[ 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 14.6   n/a MPO474699  
diameter diameter 7.435 km 0.057 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.043   0.003 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

80792 (2000 CN86)          Discovered 2000-Feb-04 by LINEAR at Socorro
Reference: 20040504/Numbers.arcLast Updated: 2004-07-16

Alternate Designations
 2000 CN86 = 2001 OQ30 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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