The angular velocity \( \omega \) of a satellite is given by:
\[
\omega = \sqrt{\frac{GM}{r^3}}
\]
Where \( G \) is the gravitational constant, \( M \) is the mass of the Earth, and \( r \) is the radius of the orbit. For two satellites at distances \( r \) and \( 2r \), the ratio of angular velocities is:
\[
\frac{\omega_1}{\omega_2} = \frac{\sqrt{\frac{GM}{r^3}}}{\sqrt{\frac{GM}{(2r)^3}}} = \frac{\sqrt{1}}{\sqrt{\frac{1}{8}}} = 2
\]
Thus, the ratio of angular velocities is \( 2:1 \).