What is the most fuel efficient method of transferring

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A satellite is ‘parked' in a circular orbit 250 km above the Earth's surface. What is the most fuel efficient method of transferring the satellite to an (elliptical) synchronous orbit by using a single impulse?

[A synchronous orbit has a period of 23 hr 56 m.] Find the value of v and apogee distance.

Reference no: EM131383091

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