I am just beginning to climb the learning curve, and so far have not located
a minor but useful function.  GMAT will take multiple ways to specify an
orbit, including state vectors/Cartesian elements, and two line elements
used in many tracking programs and supplied by Space-Track.  Is there a way
to use GMAT to do that conversion for the user?  In particular directly to
fully formatted two line elements?  There are of course a few online
sources, but their output requires considerable intermediate processing.
There are of course many packages for Python, Java, C, etc which can be
used, but I would rather not reinvent that wheel.  


Alan

-----------------------------------

Keep Calm and Carry On




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