John B. answered 10/28/22
College Physics Tutor
Kepler's third law gives the orbital period T as:
T = (2 * pi) * sqrt( a^3 / ( G * M ) )
Here,
a = magnitude of semi-major axis = radius of earth + 400km = 6771 E3 m
G = gravitational constant = 6.67E-11
M = mass of central body = 5.97E24 kg
So, plugging in these values,
T = (2 * pi) * sqrt( (6771E3)^3 / (6.67E-11 * 5.97E24) )
T = 5547 s = 1.54 hours
And for the velocity:
V = d / T = 2 pi a / T
V = ( 2 * pi * 6771E3 m ) / 5547 s
V = 7670 m/s