Changing the position of a satellite in an orbit

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Calculate the change in velocity required in changing the position of a satellite in an orbit by 90 degrees. The initial and final orbit is circular around the Earth with a 15000 km radius. Calculate the delta velocity, semi-major axis and period for a transfer orbit that will change the location by + 90 degrees and the same data to move the location by -90 degrees. The action shall use a Hohmann maneuver orbit. Calculate the total delta V required to make each change.

Reference no: EM13706759

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