# Why do satellites with greater altitude travel at a slower speed?

For example, a geostationary satellite travels slower than the ISS. What is going on?

• Have you considered looking at the force balance that keeps satellites in orbit? – AtmosphericPrisonEscape Apr 6 '17 at 0:43
• @AtmosphericPrisonEscape That is a bit misleading, there is no force balance as the only force acting on the orbiting object is gravity. – SE - stop firing the good guys Apr 6 '17 at 7:35
• @Hohmannfan: That doesn't matter. It doesn't seem to be a university-level question, and the most intuitive 'layman' way of understanding Keplerian orbits is through inertial forces. – AtmosphericPrisonEscape Apr 6 '17 at 14:48

Kepler's third law in this situation tells us that $$\frac{R^3}{P^2} = \frac{GM}{4\pi^2},$$ where $R$ is the orbital radius (or semi-major axis for an elliptical orbit), $P$ is the orbital period and $M$ is the mass of the Earth (actually, it is the mas of the Earth plus the mass of the satellite, but we can neglect the latter). Thus the orbital period $P \propto R^{3/2}$.
To calculate the orbital speed, we divide the orbital circumference by the orbital period $$v = \frac{2\pi R}{P}.$$
Then substituting for $P$ from Kepler's third law, we get $$v = \sqrt{\frac{GM}{R}}$$
Or you can just use Newton's second law and equate the centripetal acceleration to the gravitational force: $$m \frac{v^2}{R} = G\frac{Mm}{R^2},$$ where $m$ is the mass of the satellite, which leads directly to the same result.