I am a true dunce about this. Could you explain this to me in simple terms.
To move the Shuttle from its most-economical orbital orientation (i.e., it's initial post-launch orbital insertion), the Shuttle's vector for insertion has to be directed away from its optimal West-East alignment which gives it a hefty 'centrifigal' boost, and allows it to go either higher in orbit or carry more payload. PLUS a heavy series of burns of the OMS engines is required to reposition the orbit. And then, when ready to leave, this positioning with the ISSS has to be UNDONE with even more OMS burns just to get things ligned up for re-entry and landing at the Cape...