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Find the semimajor axis of a satellite orbit with an apogee altitudealtitude

 of 4,500 km and a perigee  of 500 km. (Show step-by-step).

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ec facilisis

, dictum vitaeitur laoreet


ac, dictum vitae odio. Donec aliquet. Lore

ultrices ac magna. Fusce dui lectus, congue vel laoreet ac, dictum vitae odio. Donec aliquet. Lorem ipsum dolor sit amet, consectetur adipiscing elit. Nam lacinia pulvinar tortor nec facil

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at, ultrices ac magna. Fus

m risus ante, dapibus a m


6E50192B-7BF7-44E7-9B66-64A2DEBAA3D6.jpeg

fficitur laoreet. Nam risus ante, dapibus a molestie consequat, ultrices ac magna. Fusce dui lectus, congue vel laoreet ac, dictum vitae odio. Donec aliquet. L
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