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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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .5754764946792565 0.00067998  
a 1.993917067939446 0.0028696 au
q .8464646630005128 0.00013761 au
i 4.383674664087573 0.004579 deg
node 320.1022969857804 0.0025023 deg
peri 241.529793184761 0.0011383 deg
M 197.989247353475 1.9877 deg
tp 2459463.307514762117
(2021-Sep-05.80751476)
6.6772 TDB
period 1028.392884994943
2.82
2.2201
0.006078
d
yr
n .3500607649592696 0.0007557 deg/d
Q 3.14136947287838 0.004521 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 = .011419 au 
 Jupiter MOID = 1.84964 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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