A satellite follows an elliptical orbit. The only force on the satellite is the gravity atraction from the planet. The satellites speed at point A is 8000m/s, and it is 6000km away, Point B is 24000km east of the planet, and Point C is component vector 9000ikm+12000jkm away, if the you take the planet as the origin.
a. Is there any torque acting on the satellite?
b. satellite speed at Point B
c, satellite speed at Point C
torque = force*R
The Attempt at a Solution
part a, I consider there is no torque since the only force is parallel to the pivot . Does it make sense.
part b ,since my professor does not mention gravitational force on this question , I use the f=mv^2/r to this question. i know there is no torque , and I know the radius is changing and I assume the gravitational force for at point a , b and c are the same and then I apply f=mva^2/ra = mvb^2/r2 . is that a good way to solve this problem ?