A booster launches a satellite due east from Cape Canaveral (latitude 28.5 deg N) into a 425 Km circular parking orbit. The satellite’s final orbit will be a GEO (geostationary) orbit. What maneuver(s) are required to transfer into the final orbit, and what is the total delta-V required? (Show your calculations)

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A booster launches a satellite due east from Cape Canaveral (latitude 28.5 deg N) into a 425 Km circular parking orbit.  The satellite’s final orbit will be a GEO (geostationary) orbit.  What maneuver(s) are required to transfer into the final orbit, and what is the total delta-V required?  (Show your calculations)

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