Needs to be transferred into a geostationary circular orbit

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Reference no: EM13717638

A satellite is currently in a 300 km altitude circular orbit and needs to be transferred into a geostationary circular orbit. The mission designers require the transfer to have a semi-major axis of 35,000 km. compute the required delta- v values for the general, co-planar transfer and the time of light.

Reference no: EM13717638

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