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(2014 CP13)
Classification: Apollo [NEO]          SPK-ID: 3661504
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.


Orbital Elements at Epoch 2459200.5 (2020-Dec-17.0) TDB
Reference: JPL 15 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4667060083113608 0.00025386  
a 1.891112653983358 0.00090555 au
q 1.008519015975682 2.8467e-06 au
i 4.257492591630019 0.00177 deg
node 226.0383660020693 0.0047231 deg
peri 317.6691124782192 0.002496 deg
M 213.4375291152138 0.67393 deg
tp 2459587.218372344313
(2022-Jan-07.71837234)
2.056 TDB
period 949.892651259909
2.60
0.68227
0.001868
d
yr
n .3789901938103288 0.00027222 deg/d
Q 2.773706291991035 0.0013282 au
  Orbit Determination Parameters
   # obs. used (total)      46  
   data-arc span      38 days  
   first obs. used      2014-02-10  
   last obs. used      2014-03-20  
   planetary ephem.      DE441  
   SB-pert. ephem.      SB441-N16  
   condition code      7  
   norm. resid. RMS      .42743  
   source      ORB  
   producer      Otto Matic  
   solution date      2021-Apr-15 09:20:26  

Additional Information
 Earth MOID = .0375599 au 
 Jupiter MOID = 2.1986 au 
 T_jup = 3.815 
[ 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 23.1   n/a E2014D50  

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