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How do you find the Ek of a satilite in orbit with only its mass and acceleration due to gravity?
I did something like..
Fc = Fg
mv²/r = mg <-- g = the acceleration due to gravity
but then i don't have a radius...
How do i solve this?
I did something like..
Fc = Fg
mv²/r = mg <-- g = the acceleration due to gravity
but then i don't have a radius...
How do i solve this?