Fg=Gm1m2r2Fg=\frac{Gm1m2}{r^{2}}Fg=r2Gm1m2
g=Gmr2g=\frac{Gm}{r^{2}}g=r2Gm
Ug=−Gm1m2rUg=-\frac{Gm1m2}{r}Ug=−rGm1m2
Escape Velocity: 2⋅Gmr\sqrt{\frac{2\cdot Gm}{r}}r2⋅Gm
Orbital Velocity:Gmr\sqrt{\frac{Gm}{r}}rGm
T=2πrvT=\frac{2\pi r}{v}T=v2πr
v=2πrTv=\frac{2\pi r}{T}v=T2πr
r=Gm4π23r=\sqrt[3]{\frac{Gm}{4\pi^2}}r=34π2Gm