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I need to find the orbital radius of a satilite, while only knowing its orbital period.
i tried..
a = 4π²r/T²
Fnet = Fg
a = Gm/r²
Gm/r² = 4π²r/T²
r = cuberoot(T²Gm/4π²)
didnt work out..
i tried..
a = 4π²r/T²
Fnet = Fg
a = Gm/r²
Gm/r² = 4π²r/T²
r = cuberoot(T²Gm/4π²)
didnt work out..