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JPL Small-Body Database Browser
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(2015 LF)
Classification: Apollo [NEO]          SPK-ID: 3720916
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 8 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .6649952094191796 0.00042403  
a 2.394400087916226 0.0027423 au
q .8021355000190735 9.669e-05 au
i 8.449910872078094 0.0044564 deg
node 77.28587292680686 0.00013902 deg
peri 242.030123503165 0.00081212 deg
M 6.531898520283482 0.63395 deg
tp 2458575.945537338129
(2019-Apr-02.44553734)
2.3409 TDB
period 1353.298207377848
3.71
2.3249
0.006365
d
yr
n .2660167567187845 0.000457 deg/d
Q 3.986664675813379 0.0045659 au
  Orbit Determination Parameters
   # obs. used (total)      57  
   data-arc span      1 day  
   first obs. used      2015-06-07  
   last obs. used      2015-06-08  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      7  
   norm. resid. RMS      .37042  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-14 06:13:06  

Additional Information
 Earth MOID = .000922401 au 
 Jupiter MOID = 1.45504 au 
 T_jup = 3.175 
[ 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 26.6   n/a E2015L23  

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