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Circular orbit
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In astrodynamics or celestial mechanics a circular orbit is an elliptic orbit with the eccentricity equal to 0. It is an example of a rotation around a fixed axis: this axis is the line through the center of mass perpendicular to the plane of motion.
lass="link1" onMouseover='showByLink("m2801448",this)' onMouseout='hide("m2801448")'href="http://www.absoluteastronomy.com/topics/Transverse">Transverse acceleration (perpendicular to velocity) causes change in direction.

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Encyclopedia
In astrodynamics or celestial mechanics a circular orbit is an elliptic orbit with the eccentricity equal to 0. It is an example of a rotation around a fixed axis: this axis is the line through the center of mass perpendicular to the plane of motion.
Circular acceleration
Transverse acceleration (perpendicular to velocity) causes change in direction. If it is constant in magnitude and changing in direction with the velocity, we get a circular motion. For this centripetal acceleration we have
where:
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:
Energy
Under standard assumptions, specific orbital energy is negative for a closed orbit and the orbital energy conservation equation (the Vis-viva equation) can take the form:
where:
The boundary case is which corresponds to escape from the primary (parabolic orbit), with .
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 v2 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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