Answer:
![(v)/(√(2))](https://img.qammunity.org/2020/formulas/physics/high-school/rwnkj05peqwjz9i1bariekxmet5iax4msu.png)
Step-by-step explanation:
To solve the problem, we can equate the gravitational force that keeps the satellite in orbit with the centripetal force:
![G(Mm)/(r^2)=m(v^2)/(r)](https://img.qammunity.org/2020/formulas/physics/high-school/sq2r21fwsw5j9lj803y064g7wpeetr1i55.png)
where
G is the gravitational constant
M is the mass of the planet
m is the mass of the satellite
v is the orbital speed of the satellite
r is the distance of the satellite from the planet's centre
Solving the formula for v,
![v=\sqrt{(GM)/(r)}](https://img.qammunity.org/2020/formulas/physics/high-school/e7vma7vdm1hmdh7fyj84fnxtmostf37rjz.png)
If the planet has half of the initial mass:
, the new orbital speed of the satellite will be
![v'=\sqrt{(GM')/(r)}=\sqrt{(GM)/(2r)}=(1)/(√(2))\sqrt{(GM)/(r)}=(v)/(√(2))](https://img.qammunity.org/2020/formulas/physics/high-school/m3y4wem6r1h1qaqxqr9poh1g5g7yu6dl7u.png)