Final answer:
The speed of satellite B is nine times the speed of satellite A due to their different orbital radii.
Step-by-step explanation:
When a satellite is in a circular orbit, its speed depends on the radius of the orbit. The speed is given by the formula:
v = √(GM/r)
Where:
v is the speed of the satellite
G is the gravitational constant, approximately 6.67430 × 10-11 m3 kg-1 s-2
M is the mass of the Earth, approximately 5.972 × 1024 kg
r is the orbital radius of the satellite
Using this formula, we can calculate the speed of satellite A:
vA = √(GM/rA)
The orbital radius of satellite B is nine times that of satellite A, so:
rB = 9 × rA
Substituting this value into the formula, we can calculate the speed of satellite B:
vB = √(GM/rB)
Therefore, the speed of satellite B is nine times the speed of satellite A.