Answer:
Half
Explanation:
Given that:
Now, if the satellite is moved to a distance [tex]R=4R_E[/tex]
We have the mathematical expression for the potential energy fue to gravitational field as:
[tex]U=\frac{G.M.m}{R}[/tex] ...................(1)
where:
[tex]G = 6.67\times 10^{-11}\ m^3.kg^{-1}.s^{2}[/tex]
M = mass of earth
m = mass of satellite
R = radial distance of satellite
Now from eq. (1) initially we have:
[tex]U=\frac{G.M.m}{2R_E}[/tex]
after the satellite is moved, we have:
[tex]U'=\frac{G.M.m}{4R_E}[/tex]
[tex]\Rightarrow U'=\frac{G.M.m}{2(2R_E)}[/tex]
[tex]\Rightarrow U'=\frac{1}{2} \times U[/tex]
which is half of the initial condition.