The Savior
Member
- Joined
- Mar 9, 2014
- Messages
- 48
- Gender
- Male
- HSC
- 2015
So there are 2 formulas for calculating the orbital velocity of a satellite, v= √(GM/r) and v= 2πr/T. If r was increased in the first formula, then velocity would decrease, while in the second formula, if r was increased, then velocity would increase as well. Can someone help me explain why this is? Does it have something to do with the fact that in the second formula, if r is increased, then T has to be increased as well, due to Kepler's law which states that the ratio of the cube of r to the square of t is a constant?