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JPL Small-Body Database Browser
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(2014 WE6)
Classification: Aten [NEO]          SPK-ID: 3696401
[ Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

[ hide orbit diagram ]
Orbit Diagram
[ switch to new HTML5 viewer ]

Note: This Java-based orbit viewer will eventually be retired.

Note: Make sure you have Java enabled on your browser to see the applet. This applet is provided as a 3D orbit visualization tool. The applet 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. For accurate long-term ephemerides, please instead use our Horizons system.

Note: If the applet is not working, here are some notes that might help.
Orbit Viewer

Additional Notes: the orbits shown in the applet are color coded. The planets are white lines, and the asteroid/comet is a blue line. The bright white line indicates the portion of the orbit that is above the ecliptic plane, and the darker portion is below the ecliptic plane. Likewise for the asteroid/comet orbit, the light blue indicates the portion above the ecliptic plane, and the dark blue the portion below the ecliptic plane.

Orbit Viewer applet originally written and kindly provided by Osamu Ajiki (AstroArts), and further modified by Ron Baalke (JPL).


Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1362420105270613 7.9636e-05  
a .9689275127622952 7.3647e-06 au
q .8369188803685752 8.351e-05 au
i .3391060224706632 0.0001915 deg
node 52.56804540275053 0.00072231 deg
peri 251.591118820112 0.001481 deg
M 330.6523629174999 0.0097736 deg
tp 2458628.899192912254
(2019-May-25.39919291)		 0.0097782 TDB
period 348.3656765848345
0.95		 0.0039718
1.087e-05		 d
yr
n 1.033396870579276 1.1782e-05 deg/d
Q 1.100936145156015 8.3681e-06 au
   Orbit Determination Parameters
   # obs. used (total)      25  
   data-arc span      4 days  
   first obs. used      2014-11-17  
   last obs. used      2014-11-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .74865  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:37:28  

Additional Information
 Earth MOID = .000137348 au 
 Jupiter MOID = 4.00738 au 
 T_jup = 6.225 
[ hide covariance matrix ]
Orbital Elements at Epoch 2456981.5 (2014-Nov-20.0) TDB
Reference: JPL 5 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1375498453035042 7.8088e-05  
q .835557529104664 8.0331e-05 au
tp 2456886.870971967888
(2014-Aug-17.37097197)		 0.0077577 TDB
node 52.56618664520391 0.00024158 deg
peri 251.7442397573637 0.0017111 deg
i .3416171061366274 0.00018899 deg
   Orbit Determination Parameters
   # obs. used (total)      25  
   data-arc span      4 days  
   first obs. used      2014-11-17  
   last obs. used      2014-11-21  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      4  
   norm. resid. RMS      .74865  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:37:28  

Additional Information
 Jupiter MOID = 4.00738 au 
 T_jup = 6.225 
Orbit Covariance (6×6)
  e q tp node peri i
e 6.097687541846435E-9 -6.27275050498447E-9 6.042401804266896E-7 -1.141400266068521E-10 -1.286249119254614E-7 1.471859542048871E-8
q -6.27275050498447E-9 6.453093629507366E-9 -6.213432875879484E-7 1.868321224409887E-10 1.325257537592498E-7 -1.514350273901597E-8
tp 6.042401804266896E-7 -6.213432875879484E-7 6.01820169368923E-5 8.744359083449766E-8 -1.250882376717139E-5 1.455136129262948E-6
node -1.141400266068521E-10 1.868321224409887E-10 8.744359083449766E-8 5.835900398319862E-8 5.101039383721208E-8 3.452543632999789E-10
peri -1.286249119254614E-7 1.325257537592498E-7 -1.250882376717139E-5 5.101039383721208E-8 2.927748749850884E-6 -3.147494456632921E-7
i 1.471859542048871E-8 -1.514350273901597E-8 1.455136129262948E-6 3.452543632999789E-10 -3.147494456632921E-7 3.571585598511266E-8

[ 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 30.4   n/a MPO318751  

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