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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 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 
[ hide covariance matrix ]
Orbital Elements at Epoch 2457019.5 (2014-Dec-28.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .2110902004089611 8.4089e-07  
q .662748465478367 1.0929e-06 au
tp 2457131.786532251743
(2015-Apr-19.28653225)
0.00018038 TDB
node 277.0207554845609 6.3012e-06 deg
peri 334.3842022598932 0.00014304 deg
i 3.308210679813437 1.9979e-05 deg
  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
 Jupiter MOID = 3.99275 au 
 T_jup = 6.947 
Orbit Covariance (6×6)
  e q tp node peri i
e 7.071003325267564E-13 -9.055221400687579E-13 -1.188293616102266E-10 -1.235271473159317E-12 -2.219710161280466E-12 9.650225596168134E-12
q -9.055221400687579E-13 1.194332780799156E-12 1.312885732059806E-10 1.610480733136734E-12 -2.377887720829542E-11 -1.2000275168595E-11
tp -1.188293616102266E-10 1.312885732059806E-10 3.253846395437273E-8 1.921780664500819E-10 1.639185783330587E-8 -1.836112918551757E-9
node -1.235271473159317E-12 1.610480733136734E-12 1.921780664500819E-10 3.970510582726008E-11 -5.328199677295948E-11 -7.881626543940964E-11
peri -2.219710161280466E-12 -2.377887720829542E-11 1.639185783330587E-8 -5.328199677295948E-11 2.046003305897204E-8 -2.412844272339913E-10
i 9.650225596168134E-12 -1.2000275168595E-11 -1.836112918551757E-9 -7.881626543940964E-11 -2.412844272339913E-10 3.991438882149474E-10

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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