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Circular OrbitIn astrodynamics or celestial mechanics a circular orbit is an elliptic orbit with the eccentricity equal to 0. Velocity Under standard assumptions the orbital velocity () of a body traveling along circular orbit can be computed as: -
where: Conclusion: - Velocity is constant along the path.
Orbital period Under standard assumptions the orbital period () of a body traveling along circular orbit can be computed as: -
where: Conclusions: Energy Under standard assumptions, specific orbital energy () is negative and the orbital energy conservation equation for this orbit takes the form: -
where: The virial theorem applies even without taking a time-average: - the potential energy of the system is equal to twice the total energy
- the kinetic energy of the system is equal to minus the total energy
Thus the escape velocity from any distance is √2 times the speed in a circular orbit at that distance: the kinetic energy is twice as much, hence the total energy is zero. Equation of motion Under standard assumptions, the orbital equation becomes: -
where: Delta-v to reach a circular orbit Maneuvering into a large circular orbit, e.g. a geostationary orbit, requires a larger delta-v than an escape orbit, although the latter implies getting arbitrarily far away and having more energy than needed for the orbital speed of the circular orbit. It is also a matter of maneuvering into the orbit. See also Hohmann transfer orbit. See also
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