The International Space Station orbital speed
The International Space Station orbital speed
ISS orbits about 400 km above the Earth's surface, which means that radius of its orbit is RE (Earth's radius) + 400 km.
It is easier to determine orbital speed and orbital period of satellite for circular orbits. We have satellite of mass m in a circular orbit about Earth at distance r from center of the Earth. It has centripetal acceleration directed toward the center of the Earth. Earth's gravity is the only force acting, so Newton's second law gives
Which re-arrange into vorbit = (GME / r)^1/2
To find the period of a circular orbit, we note that the satellite travels the circumference of the orbit 2πr in one period T. Using the definition of speed, we have vorbit=2πr/T, which gives T = 2πr/vorbit.
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