Earth Orbital Velocity Equation:
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The orbital velocity is the speed needed to balance Earth's gravity and maintain a stable orbit at a given altitude. It depends on the distance from Earth's center.
The calculator uses the orbital velocity equation:
Where:
Explanation: The equation balances gravitational force with centripetal force required for circular orbit.
Details: Calculating orbital velocity is essential for satellite deployment, space mission planning, and understanding orbital mechanics.
Tips: Enter the orbital radius in meters (distance from Earth's center). For altitude above Earth's surface, add Earth's radius (~6,371 km).
Q1: What's the orbital velocity at Earth's surface?
A: Approximately 7.9 km/s (first cosmic velocity), though atmospheric drag makes this impractical.
Q2: How does velocity change with altitude?
A: Velocity decreases with increasing altitude (lower at higher orbits).
Q3: What's geostationary orbit velocity?
A: At ~35,786 km altitude, orbital velocity is about 3.07 km/s.
Q4: Does this account for elliptical orbits?
A: No, this calculates circular orbit velocity. Elliptical orbits have varying velocity.
Q5: What about other celestial bodies?
A: Replace Earth's mass with the mass of the other body to calculate its orbital velocity.