TEMEToPEF:

Path: Orbit/OrbitCoord

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   Computes the matrix from TEME to the pseudo-earth fixed frame.
   Equivalent to a rotation about the Z axis by GMST.
   TEME is the true equator, mean equinox frame of satellite ephemerides
   generated from TLEs using SGP4 propagation.

   Since version 9.
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   Form:
   c = TEMEToPEF( jD )	
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   ------
   Inputs
   ------
   jD            Julian date

   -------
   Outputs
   -------
   c		          Matrix from TEME to planet fixed

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   References:   Vallado
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Children:

Common: Time/JD2000
Common: Transform/Eul2Mat
OrbitMiniToolbox: Support/GMSTime

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