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JPL Small-Body Database Browser
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(2014 YE15)
Classification: Aten [NEO]          SPK-ID: 3703059
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 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2061430041498741 8.2279e-07  
a .8448109581071801 6.1098e-07 au
q .6706590892642325 1.146e-06 au
i 3.22430666183589 1.963e-05 deg
node 276.6276405383909 2.7581e-05 deg
peri 333.2553843137789 0.00019041 deg
M 64.29776440262197 0.0018867 deg
tp 2458549.843975077591
(2019-Mar-07.34397508)
0.0014318 TDB
period 283.6205759484193
0.78
0.00030768
8.424e-07
d
yr
n 1.269301420731447 1.377e-06 deg/d
Q 1.018962826950128 7.3693e-07 au
  Orbit Determination Parameters
   # obs. used (total)      42  
   # delay obs. used      3  
   # Doppler obs. used      5  
   data-arc span      4 days  
   first obs. used      2014-12-26  
   last obs. used      2014-12-30  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      3  
   norm. resid. RMS      .51892  
   source      ORB  
   producer      Otto Matic  
   solution date      2019-Jul-18 07:27:15  

Additional Information
 Earth MOID = .00350229 au 
 Jupiter MOID = 3.99314 au 
 T_jup = 6.947 
[ 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 28.3   n/a MPO319071  

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