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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 2459000.5 (2020-May-31.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2060780765230049 8.2921e-07  
a .8447780788438405 6.0834e-07 au
q .6706878372669025 1.1497e-06 au
i 3.22432132537827 1.9674e-05 deg
node 276.6091544299572 2.4265e-05 deg
peri 333.2674207199211 0.000188 deg
M 212.0502224964441 0.0024323 deg
tp 2459117.053198529476
(2020-Sep-24.55319853)
0.0020416 TDB
period 283.6040187326612
0.78
0.00030634
8.387e-07
d
yr
n 1.269375524397464 1.3712e-06 deg/d
Q 1.018868320420778 7.3371e-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 = .00345822 au 
 Jupiter MOID = 3.99275 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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