Solve the problem.A space shuttle is in a circular orbit 250 km above the Earth's surface. Use Kepler's third law( with
) to find the orbital period of the satellite.(G = 6.67 × 10-11 Nm2 kg-2, M = 5.97 × 1024 kg and Earth's radius is
).
A. T = 2 hr
B. T = 9 min
C. T = 1 hr
D. T = 90 min
Answer: D
Mathematics
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