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17015 (1999 CN117)
Classification: Main-belt Asteroid          SPK-ID: 2017015
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 25 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .110670484073696 3.1181e-08  
a 2.215133215020775 6.0771e-09 au
q 1.969983349826703 7.0373e-08 au
i 3.581924491348168 3.6176e-06 deg
node 187.4773360413774 5.0904e-05 deg
peri 60.5798062272516 5.3362e-05 deg
M 84.89412399393431 1.5755e-05 deg
tp 2458716.529431295150
(2019-Aug-21.02943130)
5.2535e-05 TDB
period 1204.198829368336
3.30
4.9554e-06
1.357e-08
d
yr
n .29895395280266 1.2302e-09 deg/d
Q 2.460283080214847 6.7496e-09 au
  Orbit Determination Parameters
   # obs. used (total)      2028  
   data-arc span      10915 days (29.88 yr)  
   first obs. used      1990-09-16  
   last obs. used      2020-08-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      0  
   norm. resid. RMS      .48604  
   source      ORB  
   producer      Otto Matic  
   solution date      2020-Aug-25 01:10:32  

Additional Information
 Earth MOID = .959338 au 
 Jupiter MOID = 2.55347 au 
 T_jup = 3.643 
[ 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 14.3   n/a MPO384900  
diameter diameter 3.862 km 0.218 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  
geometric albedo albedo 0.326   0.023 urn:nasa:pds:neowise_diameters_albedos::2.0[mainbelt] (http://adsabs.harvard.edu/abs/2011ApJ...741...68M)  

17015 (1999 CN117)          Discovered 1999-Feb-12 by LINEAR at Socorro
Reference: 20000913/Numbers.arcLast Updated: 2004-04-19

Alternate Designations
 1999 CN117 = 1990 SP18 = 1996 FF23 = 1997 RB2 = 1999 FU59 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Discovery Circumstances ]
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