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Orbital Eccentricity

from Continuum by Ladd Allen Doane

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Orbital Eccentricity

The orbital eccentricity of an astronomical object is a parameter that determines the amount by which its orbit around another body deviates from a perfect circle. A value of 0 is a circular orbit, values between 0 and 1 form an elliptic orbit, 1 is a parabolic escape orbit, and greater than 1 is a hyperbola. The term derives its name from the parameters of conic sections, as every Kepler orbit is a conic section. It is normally used for the isolated two-body problem, but extensions exist for objects following a Klemperer rosette orbit through the galaxy.

en.wikipedia.org/wiki/Orbital_eccentricity

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from Continuum, track released February 7, 2019

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Ladd Allen Doane

Transcendental rhythms and soundscapes hover over one another causing fractions of time to stand still.

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