The International Space Station makes 1565 revolutions per d

The International Space Station makes 15.65 revolutions per day in its orbit around the earth. Assuming a circular orbit, how high is this satellite above the surface of the earth?

Solution

First, we need the period in sec

T = 24(3600)/15.65

T = 5521 sec per rev

Then by Kepler\'s Third Law

T2/r3 = 4pi2/GM

(5521)2/r3 = 4pi2/(6.67 X 10-11)(5.98 X 1024)

r = 67528765 m from the center of the Earth

From the suface, subtract the radius of the Earth

67528765 - 6.38 X 106 = 372875 m

Divide by 1000 for answer in km

That is 373 km (Rounding to three sig figs)


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