Step 1: Use the formula of centripetal acceleration.
Centripetal acceleration is given by
\[
a_c=\omega^2r
\]
where
\[
\omega
\]
is angular speed and
\[
r
\]
is radius.
Step 2: Substitute the given values.
Given,
\[
a_c=10\,\text{ms}^{-2}
\]
and
\[
r=10\,\text{m}
\]
So,
\[
10=\omega^2(10)
\]
\[
\omega^2=1
\]
\[
\omega=1
\]
Since angular speed is positive,
\[
\omega=1\,\text{rad s}^{-1}
\]
Step 3: Final conclusion.
Hence, the angular speed of the satellite is
\[
\boxed{1\,\text{rad s}^{-1}}
\]