Final answer:
The orbital velocity of satellite Y is 2 times the orbital velocity of satellite X.
Step-by-step explanation:
The orbital velocity of satellite Y can be determined using the concept of conservation of angular momentum. The angular momentum of a satellite is given by the equation:
L = mvr
where L is the angular momentum, m is the mass of the satellite, v is the orbital velocity, and r is the radius of the orbit. Since both satellites are at the same height, the radius of their orbits would be the same. Therefore, the angular momentum of satellite Y would be:
LY = 2m * v * r
Using the equation for angular momentum of satellite X (LX = m * v * r), we can compare the two angular momenta:
LY / LX = (2m * v * r) / (m * v * r) = 2
Since angular momentum is conserved, the ratio of the angular momenta is equal to the ratio of the masses. Therefore, the orbital velocity of satellite Y would be equal to 2 times the orbital velocity of satellite X. So the correct answer is b) 2v.