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A booster launches a satellite due east from a launch center ( 19.4 degrees North, 110.6 degrees East) into a 200 Km circular parking orbit.

A booster launches a satellite due east from a launch center ( 19.4 degrees North, 110.6 degrees East) into a 200 Km circular parking orbit. The satellite's final orbit will be a GEO orbit. What maneuver (s) are required to transfer into the final orbit, and what is the total delta-V required ? Draw a diagram of the maneuver.

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