Orbit Velocity Equation:
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Orbit velocity is the speed needed for an object to maintain a stable orbit around a celestial body. It depends on the standard gravitational parameter of the body being orbited and the orbital radius.
The calculator uses the orbit velocity equation:
Where:
Explanation: The equation shows that orbital velocity decreases with increasing orbital radius and increases with greater gravitational force.
Details: Calculating orbit velocity is essential for satellite deployment, space mission planning, and understanding celestial mechanics. It determines the speed required to maintain a stable orbit without falling back to the surface or escaping the gravitational pull.
Tips: Enter the standard gravitational parameter in m³/s² and orbital radius in meters. Both values must be positive numbers. For Earth, gm ≈ 3.986×10¹⁴ m³/s².
Q1: What's the difference between orbital velocity and escape velocity?
A: Orbital velocity maintains a stable orbit, while escape velocity is the speed needed to completely break free from a gravitational field.
Q2: How does altitude affect orbital velocity?
A: Higher orbits (greater r) have slower orbital velocities. Low Earth orbit requires about 7.8 km/s, while geostationary orbit requires about 3.1 km/s.
Q3: What is the standard gravitational parameter?
A: It's the product of the gravitational constant (G) and the mass of the celestial body (M), often denoted as μ (mu) or gm in equations.
Q4: Does this equation work for circular orbits only?
A: This equation gives the circular orbit velocity. For elliptical orbits, the velocity varies throughout the orbit.
Q5: How accurate is this calculation for real-world applications?
A: This provides the theoretical value. Real-world factors like atmospheric drag, non-spherical gravity fields, and other celestial bodies' influence may require adjustments.