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Geostationary Orbit Calculator

Compute synchronous orbit radius r = (GM T²/4π²)^{1/3}.

Input Data

Input Rotation period T.
s
Input Central mass M.
kg

Results

42,163,743.57m
r = (GM T²/4π²)^{1/3} = 42163743.57 m

At a glance:Geostationary Orbit Calculator: enter parameters to compute results; complements related calculators.

Formula

r = (G M T² / 4π²)^{1/3}

G=6.67430×10⁻¹¹, T: rotation period

How to Use

  1. Enter rotation period T (sidereal day, Earth≈86164 s).
  2. Enter central mass M.
  3. Get synchronous orbit radius r.

Case Studies

Earth

T=86164 s, M=5.972×10²⁴ kg → r≈4.216×10⁷ m (≈42164 km).

FAQ

Why sidereal day?

Synchrony is against inertial space, so use the sidereal day, not solar.

Related Tools

References

Content review: Calculatorism Science Team. Formula and numeric tests verified; results for reference only.

Found a problem with the results?

If this calculator's result is wrong, or you have any question about the calculation logic, please let us know. You are viewing:Geostationary Orbit Calculator/physics/geostationary-orbit)。