Orbital speed is the velocity a body needs to stay in a stable orbit around another body due to gravitational forces. It depends on the masses of both objects and the distance between them.
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Orbital speed decreases with increasing altitude from the primary body.
Kepler's Third Law relates orbital period to the semi-major axis of an orbit, indirectly involving orbital speed.
For circular orbits, orbital speed is constant; for elliptical orbits, it varies.
Orbital speed at a given point can be calculated using the formula v = √(GM/r), where G is the gravitational constant, M is the mass of the primary body, and r is the distance from its center.
Geostationary satellites have an orbital speed that matches Earth's rotation.
Review Questions
What happens to orbital speed as altitude increases?
How does Kepler's Third Law relate to orbital speed?
What is the formula for calculating orbital speed?