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Gravity Challenge #5 — Geostationary Orbits

The height of a
geostationary orbit.

Gravity Hard

Problem

A geostationary satellite circles Earth exactly once every 86,400 s, hovering over one spot on the equator. Calculate its height above Earth’s surface, in kilometres.

  • Orbital period\( T = 86{,}400\ \mathrm{s} \)
  • Earth’s GM\( 4.0 \times 10^{14}\ \mathrm{m^3/s^2} \)
  • Earth’s radius\( R_E = 6.4 \times 10^6\ \mathrm{m} \)
  • Answer inkilometres
Height means above the surface — the orbit radius is measured from Earth’s centre.
Hint: gravity supplies the centripetal force with \( \omega = \tfrac{2\pi}{T} \), which packs into \( r^3 = \tfrac{GMT^2}{4\pi^2} \). Cube-root for \( r \) — then remember what the question asked for.
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