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JPL Small-Body Database Browser
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(2015 YE1)
Classification: Apollo [NEO]          SPK-ID: 3738915
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 .3206503672699577 0.00022538  
a 1.20388337915182 0.00028313 au
q .817857731476591 7.8991e-05 au
i 10.13816291958282 0.006775 deg
node 86.08679798838889 7.13e-05 deg
peri 77.71895921419133 0.0021268 deg
M 150.2015040050831 0.29885 deg
tp 2458399.198581411236
(2018-Oct-07.69858141)
0.32951 TDB
period 482.4752666225137
1.32
0.1702
0.000466
d
yr
n .7461522380621062 0.00026322 deg/d
Q 1.589909026827048 0.00037391 au
  Orbit Determination Parameters
   # obs. used (total)      61  
   data-arc span      4 days  
   first obs. used      2015-12-18  
   last obs. used      2015-12-22  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .48726  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:29:42  

Additional Information
 Earth MOID = .0143738 au 
 Jupiter MOID = 3.41483 au 
 T_jup = 5.219 
[ 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 27.4   n/a MPO358619  

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