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160205 (2002 CF35)
Classification: Main-belt Asteroid          SPK-ID: 2160205
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 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1758949677792694 5.8148e-08  
a 2.571968270697097 2.0504e-08 au
q 2.119571994593528 1.558e-07 au
i 13.91781699782472 6.6337e-06 deg
node 30.75591329430565 1.6936e-05 deg
peri 239.041156939556 2.3487e-05 deg
M 56.14140636297936 1.6163e-05 deg
tp 2458765.548823729329
(2019-Oct-09.04882373)
6.7055e-05 TDB
period 1506.596092562739
4.12
1.8016e-05
4.933e-08
d
yr
n .2389492457713968 2.8574e-09 deg/d
Q 3.024364546800666 2.4111e-08 au
  Orbit Determination Parameters
   # obs. used (total)      653  
   data-arc span      7775 days (21.29 yr)  
   first obs. used      1998-03-24  
   last obs. used      2019-07-07  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .58573  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Feb-24 13:15:49  

Additional Information
 Earth MOID = 1.14108 au 
 Jupiter MOID = 2.14427 au 
 T_jup = 3.367 
[ 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 15.1   n/a MPO338314  
diameter diameter 2.713 km 0.329 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.288   0.127 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

160205 (2002 CF35)          Discovered 2002-Feb-06 by LINEAR at Socorro
Reference: 20070730/Numbers.arcLast Updated: 2007-08-06

Alternate Designations
 2002 CF35 = 1998 FB89 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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