Orbital Velocity

📊 advanced

$$v_o = \sqrt{\frac{GM}{r}}$$

Velocity required for a satellite to stay in a circular orbit.

Variables & Units

$v_o$

Orbital Velocity

Unit: $m/s$

Key Information

📐 Derived From

Gravitational force = Centripetal force.

💡 Example

Velocity of the ISS.

🔧 Applications

Telecommunications satellites.

⚠️ Constraints

Circular orbit assumed.

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