You wish to place a spacecraft in a circular orbit around the earth so that its orbital speed will be 4.00 * 10^3 m/s. What are this orbit’s (a) radius, (b) altitude above the earth’s surface, and (c) period (in hours)?
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You wish to place a spacecraft in a circular orbit around the
earth so that its orbital speed will be 4.00 * 10^3 m/s. What are this orbit’s
(a) radius, (b) altitude above the earth’s surface, and (c) period (in hours)?
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