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(2014 CE)
Classification: Apollo [NEO]          SPK-ID: 3660383
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 12 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4575514706220705 9.4588e-05  
a 1.369918012463936 0.0001725 au
q .7431100112293983 3.601e-05 au
i 6.043509004363417 0.0011821 deg
node 133.0314855915711 0.00011041 deg
peri 281.2372612189321 0.00032775 deg
M 11.69001968224788 0.28319 deg
tp 2458981.482517181071
(2020-May-11.98251718)
0.45711 TDB
period 585.6528903207009
1.60
0.11062
0.0003029
d
yr
n .6146985799094505 0.00011611 deg/d
Q 1.996726013698474 0.00025143 au
  Orbit Determination Parameters
   # obs. used (total)      57  
   data-arc span      26 days  
   first obs. used      2014-02-02  
   last obs. used      2014-02-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .32452  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:42:35  

Additional Information
 Earth MOID = .00223422 au 
 Jupiter MOID = 3.39049 au 
 T_jup = 4.706 
[ 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 26.9   n/a MPO292223  

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