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JPL Small-Body Database Browser
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(2013 CE82)
Classification: Apollo [NEO]          SPK-ID: 3626395
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


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Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .575656006098163 0.00067595  
a 1.993871150964349 0.0028863 au
q .8460872475258642 0.00012296 au
i 4.384026089061085 0.0045628 deg
node 320.1085478728704 0.0022657 deg
peri 241.5288013603326 0.00055509 deg
M 57.93106253657245 1.6854 deg
tp 2458435.017126036142
(2018-Nov-12.51712604)
4.4551 TDB
period 1028.357361637884
2.82
2.233
0.006114
d
yr
n .350072857383567 0.00076015 deg/d
Q 3.141655054402833 0.0045479 au
  Orbit Determination Parameters
   # obs. used (total)      38  
   data-arc span      11 days  
   first obs. used      2013-02-05  
   last obs. used      2013-02-16  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .60445  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:46:52  

Additional Information
 Earth MOID = .0113921 au 
 Jupiter MOID = 1.8504 au 
 T_jup = 3.619 
[ 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 24.6   n/a MPO258453  

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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