To transfer a satellite from an elliptical orbit to a circular orbit h – McqOptions

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1.	To transfer a satellite from an elliptical orbit to a circular orbit having radius equal to the apogee distance of the elliptical orbit, the speed of the satellite should be
A.	increased at the apogee
B.	decreased at the apogee
C.	increased at the perigee
D.	decreased at the perigee
Answer» B. decreased at the apogee

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