To find the new velocity of a satellite when it is moved to an orbital radius of \(5r\), we can use the formula for the orbital speed 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.
When the orbital radius is changed to \(5r\), the new velocity \(v'\) will be:
\[ v' = \sqrt{\frac{GM}{5r}} = \sqrt{\frac{1}{5}} \sqrt{\frac{GM}{r}} = \frac{1}{\sqrt{5}} v \]
Thus, the correct response that represents the velocity of the satellite when moved to an orbital radius of \(5r\) is:
\(\frac{1}{\sqrt{5}} v\)
So, the answer is:
1/√5 v