Homework Statement
Show that a satellite in low-Earth orbit is approximately P = C(1 + 3h/2R_E) where h is the height of the satellite, C is a constant, and R_E is the radius of the earth)
Homework Equations
p=C(1+3H/2R_E)
p2 = (4∏2)/(GM) * a3. (G - gravitational constant, M - mass of the...