satellite needs to move into a circular orbit with r 12500 km. 1. What is the minimum total Av required to complete this transfer? 2. How long will it take the satellite to complete the transfer?

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A satellite is in an initial orbit with apogee radius, r.= 7500 km and perigee radius, r, 7000 km. The
satellite needs to move into a circular orbit with r= 12500 km.
%3D
1. What is the minimum total Av required to complete this transfer?
2. How long will it take the satellite to complete the transfer?
Transcribed Image Text:A satellite is in an initial orbit with apogee radius, r.= 7500 km and perigee radius, r, 7000 km. The satellite needs to move into a circular orbit with r= 12500 km. %3D 1. What is the minimum total Av required to complete this transfer? 2. How long will it take the satellite to complete the transfer?
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