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JPL Small-Body Database Browser
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(2014 YT15)
Classification: Apollo [NEO]          SPK-ID: 3703074
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 4 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .1300221803692587 6.9283e-05  
a 1.057791051795976 6.2253e-05 au
q .9202547528663716 2.6959e-05 au
i 9.835089431549733 0.0049485 deg
node 96.01074018100421 0.00032726 deg
peri 68.92572111601001 0.010143 deg
M 297.067197649777 0.11386 deg
tp 2458669.966086114492
(2019-Jul-05.46608611)
0.13181 TDB
period 397.3729131280057
1.09
0.035079
9.604e-05
d
yr
n .9059500235337712 7.9975e-05 deg/d
Q 1.19532735072558 7.0347e-05 au
  Orbit Determination Parameters
   # obs. used (total)      36  
   data-arc span      1 day  
   first obs. used      2014-12-28  
   last obs. used      2014-12-29  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .44669  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:36:40  

Additional Information
 Earth MOID = .00866738 au 
 Jupiter MOID = 3.78906 au 
 T_jup = 5.800 
[ 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 27.2   n/a MPO319071  

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