To determine the velocity \( v' \) of a satellite moved from an orbital radius \( r \) to an orbital radius of \( 5r \), we can use the formula for the orbital velocity of a satellite, which is given by:
\[ v = \sqrt{\frac{GM}{r}} \]
where \( G \) is the gravitational constant and \( M \) is the mass of the Earth.
For the new orbital radius \( 5r \):
\[ v' = \sqrt{\frac{GM}{5r}} = \sqrt{\frac{1}{5}} \sqrt{\frac{GM}{r}} = \frac{1}{\sqrt{5}} v \]
Thus, the velocity of the satellite at the orbit of radius \( 5r \) is:
\[ v' = \frac{1}{\sqrt{5}} v \]
So, the correct response is:
1/5√v