OrbitFromSynodic:

Path: Orbit/OrbitMechanics

% Computes the elements of an orbit with the desired synodic period.

   Type OrbitFromSynodic for a demo.

   Since version 2014.1
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   Form:
   el = OrbitFromSynodic( elT, p, mu, h )
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   ------
   Inputs
   ------
   el            (1,6)   Target orbit [a i W w e M]
   p             (1,1)   Desired synodic period
   mu            (1,1)   Gravitational constant
   h             (1,1)   Any entry get a higher orbit

   -------
   Outputs
   -------
   el            (1,6)   Orbit [a i W w e M]

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Children:

Common: Database/Constant
Common: Graphics/Plot2D
Orbit: OrbitMechanics/RVOrbGen
SC: BasicOrbit/Period

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