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JPL Small-Body Database Browser
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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 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 12 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4577917172648415 9.5206e-05  
a 1.369905204329102 0.00017181 au
q .7427739483492386 3.7269e-05 au
i 6.04242426765768 0.0011825 deg
node 133.0511118915937 9.7733e-05 deg
peri 281.1977236597135 0.0003275 deg
M 125.8698138716446 0.23683 deg
tp 2458395.736148662211
(2018-Oct-04.23614866)
0.34676 TDB
period 585.6446769419612
1.60
0.11018
0.0003017
d
yr
n .6147072007548988 0.00011564 deg/d
Q 1.997036460308965 0.00025047 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 = .00228369 au 
 Jupiter MOID = 3.3891 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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