For a satellite orbiting just above the surface of the Earth, we can use the formula for the period T of the satellite in terms of the Earth's density d and the gravitational constant G:
where a is the semi-major axis of the orbit (which is approximately equal to the Earth's radius R for a satellite orbiting just above the surface) and M is the mass of the Earth.
We can express the mass of the Earth M in terms of its density d and volume:
Now, substitute this expression for M into the equation for T:
Since the satellite is orbiting just above the Earth's surface, we can approximate a ≈ R:
Simplify the equation:
Now, square both sides of the equation:
Simplify further:
Thus, the quantity
represents
.