Answer:
r = 2.8524 x10⁷ m = 28524 km
Explanation:
First, we calculate the angular speed of the satellite:
[tex]\omega = \frac{Arc Length}{Time}\\\\For\ One\ Complete\ Revolution\ around\ Cruton:\\\\\omega = \frac{2\pi\ rad}{5.82\ h}\frac{1\ h}{3600\ s}\\\omega = 3\ x\ 10^{-4} rad/s[/tex]
Now, we use the formula for the gravitational force. Since gravitational force will be acting as the centrifugal force due to circular motion. Therefore,
[tex]F = \frac{mv^{2}}{r}\\[/tex]
where,
F = Gravitational Forc = 105 N
m = mass of satellite = 40.9 kg
v = linear speed of satellite = rω = r(3 x 10⁻⁴ rad/s)
r = radius of orbit = ?
Therefore,
[tex]105\ N = \frac{(40.9\ kg)(r*3\ x\ 10^{-4}\ rad/s)^{2}}{r}\\r = \frac{105}{(40.9)(9\ x\ 10^{-8})} \\[/tex]
r = 2.8524 x10⁷ m = 28524 km