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(2014 CB3)
Classification: Apollo [NEO]          SPK-ID: 3661318
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 7 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2638717483112183 0.00043329  
a 1.299974431900324 0.00069896 au
q .9569479057949026 4.8791e-05 au
i 10.04019745919238 0.01438 deg
node 318.2348806857066 0.0015965 deg
peri 223.5084623536478 0.0044273 deg
M 66.32575337045003 1.2664 deg
tp 2458900.757480639523
(2020-Feb-21.25748064)
1.824 TDB
period 541.3780491752287
1.48
0.43663
0.001195
d
yr
n .6649697019457067 0.00053631 deg/d
Q 1.643000958005745 0.0008834 au
  Orbit Determination Parameters
   # obs. used (total)      38  
   data-arc span      4 days  
   first obs. used      2014-02-06  
   last obs. used      2014-02-10  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .4424  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:42:34  

Additional Information
 Earth MOID = .021401 au 
 Jupiter MOID = 3.34087 au 
 T_jup = 4.952 
[ 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 26.1   n/a MPO284143  

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