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(2005 CR16)
Classification: Centaur          SPK-ID: 3268479
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ show orbit diagram ]
Orbital Elements at Epoch 2459000.5 (2020-May-31.0) TDB
Reference: JPL 3 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5098423138487955 1.9845e-05  
a 6.623839516432899 0.00029389 au
q 3.246725850811663 1.2781e-05 au
i 9.393851370746189 5.4675e-05 deg
node 139.9852321903741 0.00014598 deg
peri 313.1302540730925 0.003055 deg
M 337.4413023866163 0.021936 deg
tp 2459390.688667296601
(2021-Jun-25.18866730)
0.40536 TDB
period 6226.774374751088
17.05
0.41441
0.001135
d
yr
n .05781484575059632 3.8477e-06 deg/d
Q 10.00095318205414 0.00044373 au
  Orbit Determination Parameters
   # obs. used (total)      38  
   data-arc span      502 days (1.37 yr)  
   first obs. used      2003-11-19  
   last obs. used      2005-04-04  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .66292  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-08 20:50:07  

Additional Information
 Earth MOID = 2.27334 au 
 Jupiter MOID = .421808 au 
 T_jup = 2.701 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 14.0   n/a MPO132989  

[ show close-approach data ]
Alternate Designations
 2005 CR16 = 2003 WR168 
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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