Fg=Gm1m2r2Fg=\frac{Gm1m2}{r^{2}}Fg=r2Gm1m2β
g=Gmr2g=\frac{Gm}{r^{2}}g=r2Gmβ
Ug=βGm1m2rUg=-\frac{Gm1m2}{r}Ug=βrGm1m2β
Escape Velocity: 2β Gmr\sqrt{\frac{2\cdot Gm}{r}}r2β Gmββ
Orbital Velocity:Gmr\sqrt{\frac{Gm}{r}}rGmββ
T=2ΟrvT=\frac{2\pi r}{v}T=v2Οrβ
v=2ΟrTv=\frac{2\pi r}{T}v=T2Οrβ
r=Gm4Ο23r=\sqrt[3]{\frac{Gm}{4\pi^2}}r=34Ο2Gmββ