An earth orbit has a perigee radius of 7000 km and a


An earth orbit has a perigee radius of 7000 km and a perigee velocity of 9 km/s. Calculate the change in apogee radius due to a change of

(a) 1 km in the perigee radius.

(b) 1 m/s in the perigee speed.

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Microeconomics: An earth orbit has a perigee radius of 7000 km and a
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