
William W. answered 12/30/20
Experienced Tutor and Retired Engineer
A variation of Kepler's third law is:
allowing you to solve for the period of an orbiting object.
T is the period of the ISS, G is the universal gravitational constant which is 6.674 x 10−11 m3/(kg s2), ME is the mass of earth (given in your problem as 5.98 x 1024 kg) and r is the radius of the ISS (radius of the earth plus the altitude of the ISS which is given in your problem as 6.77 x 106 m)
So T = (2π/√(6.674 x 10−11•5.98 x 1024))(6.77 x 106)3/2
T = 5540 seconds and to convert to hours, one hour is 3600 seconds so 5540/3600 = 1.54 hours