Orbital Velocity Equation:
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Orbital velocity is the speed at which a satellite or other body travels around another body in a stable orbit. It depends on the mass of the central body and the distance from its center.
The calculator uses the orbital velocity equation:
Where:
Explanation: The equation shows that orbital velocity decreases with increasing orbital radius and increases with greater gravitational parameter.
Details: Calculating orbital velocity is essential for satellite deployment, space mission planning, and understanding celestial mechanics.
Tips: Enter the standard gravitational parameter (μ) in m³/s² and orbital radius in meters. Both values must be positive numbers.
Q1: What is the standard gravitational parameter (μ)?
A: It's the product of the gravitational constant (G) and the mass of the celestial body (M). For Earth, μ ≈ 3.986×10¹⁴ m³/s².
Q2: Does this work for circular orbits only?
A: This equation gives the circular orbital velocity. For elliptical orbits, the velocity varies throughout the orbit.
Q3: What units should I use?
A: Use meters for distance and m³/s² for μ to get velocity in m/s.
Q4: How does altitude affect orbital velocity?
A: Higher altitude (greater r) results in lower orbital velocity.
Q5: Can I use this for planets orbiting the Sun?
A: Yes, using the Sun's gravitational parameter (μ ≈ 1.327×10²⁰ m³/s²).