Orbital eccentricity is a dimensionless parameter describing how much an orbit's shape deviates from a perfect circle. A value of 0 is a circular orbit, values between 0 and 1 describe an ellipse, exactly 1 describes a parabolic escape or capture trajectory, and values greater than 1 describe a hyperbolic trajectory that will never return. It is one of the six classical orbital elements, alongside inclination, and follows directly from Johannes Kepler's description of planetary orbits as ellipses.
Facts
Concept Domain Formulated Year Proposed ByKepler's first law, published in Astronomia Nova (1609), established that planetary orbits are ellipses rather than circles, which is what eccentricity quantifies. Connections
Associated With
Source Wikipedia (space and spaceflight articles)
Source Wikipedia (space and spaceflight articles)
Additional Source Astronomia nova (Wikipedia)Astronomia nova article, lead section
Source Wikipedia (space and spaceflight articles)
Source Wikipedia (space and spaceflight articles)
Sources
1. Wikipedia (space and spaceflight articles)
Wikimedia Foundation- Associated With: Orbital Mechanics
- Associated With: Heliocentrism
- Associated With: Orbital Inclination
View the Source 2. Encyclopedia Britannica: Space Exploration
Orbital eccentricity (Wikipedia)
Orbital eccentricity, lead section
A value of 0 is a circular orbit, values between 0 and 1 form an elliptic orbit, 1 is a parabolic (escape orbit or capture orbit), and greater than 1 is a hyperbola.
In Group: Orbital Elements and Celestial Mechanics, Lead sentence
In astrodynamics, the orbital eccentricity of an astronomical object is a dimensionless parameter that determines the amount by which its orbit around another body deviates from a perfect circle.
View the SourceAstronomia nova (Wikipedia)
Astronomia nova article, lead sectionQuote, Astronomia nova article, lead section
is a book, published in 1609, that contains the results of the astronomer Johannes Kepler's ten-year-long investigation of the motion of Mars.
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