MoonEl:

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   Computes the moon orbital elements with respect to the
   earth inertial frame.

   These elements are only valid for short term use. Use PlanetPosJPL
   for more accurate positions and velocities.

   Since version 2.
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   Form:
   el = MoonEl( jD )
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   Inputs
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   jD            (1,1)  Julian Date

   -------
   Outputs
   -------
   el            (1,6)  Keplerian elements [a,i,L,w,e,M] (km,rad)

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   Reference: Montenbruck, O., T. Fleger, "Astronomy on the Personal 
               Computer", Springer-Verlag, p 155.
               http://ssd.jpl.nasa.gov/?sat_elem
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Children:

Common: Time/JD2T