Recent content by jeanbeanie

  1. J

    Showing that a near earth orbit is P = C(1 + 3h/2R_E)

    we have never done anything like this, I am not even sure were to start with it
  2. J

    Showing that a near earth orbit is P = C(1 + 3h/2R_E)

    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...