CEcl2SER:

Path: Orbit/OrbitCoord

% Transformation matrix from ecliptic to Sun-Earth rotating frame.
   This is a single rotation about the z-axis. If the JD is not input it
   will use the ecliptic longitude for J2000.0.

   Since version 2014.1
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   Form:
   c = CEcl2SER( jD )
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   ------
   Inputs
   ------
   jD            (1,1)    Julian date

   -------
   Outputs
   -------
   c             (3,3)    Transformation matrix from the heliocentric
                           frame with xy ecliptic plane to Sun-Earth
                           rotating frame, with x along Sun-Earth line, y
                           orthoganal to xz plane.

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