Answer:
The speed of satellite moving into circular orbit of radius 4R will become half of the speed of satellite moving into circular orbit of radius R.
Explanation:
Speed of satellite revolving around the central body in a circular path:

Where :
G = gravitational constant = ![6.673 \times 10^{-11} Nm^2/kg^2]](https://tex.z-dn.net/?f=6.673%20%5Ctimes%2010%5E%7B-11%7D%20Nm%5E2%2Fkg%5E2%5D)
M = Mass of body around which satellite is orbiting
R = radius of the orbit from the satellite
A satellite originally moves in a circular orbit of radius R around the Earth.The velocity of satellite will be ;
..[1]
If the same satellite moves in a circular orbit of radius $R around the Earth.The speed of satellite will be :
..[2]
Dividing [1] and [2]:



The speed of satellite moving into circular orbit of radius 4R will become half of the speed of satellite moving into circular orbit of radius R.