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Elliptic orbit and Kepler orbit

Shortcuts: Differences, Similarities, Jaccard Similarity Coefficient, References.

Difference between Elliptic orbit and Kepler orbit

Elliptic orbit vs. Kepler orbit

In astrodynamics or celestial mechanics, an elliptic orbit or elliptical orbit is a Kepler orbit with an eccentricity of less than 1; this includes the special case of a circular orbit, with eccentricity equal to 0. In celestial mechanics, a Kepler orbit (or Keplerian orbit) is the motion of one body relative to another, as an ellipse, parabola, or hyperbola, which forms a two-dimensional orbital plane in three-dimensional space.

Similarities between Elliptic orbit and Kepler orbit

Elliptic orbit and Kepler orbit have 18 things in common (in Unionpedia): Apsis, Asteroid, Barycenter, Celestial mechanics, Ellipse, Gravitational two-body problem, Hyperbolic trajectory, Isaac Newton, Johannes Kepler, Kepler's laws of planetary motion, Newton's law of universal gravitation, Orbital eccentricity, Orbital elements, Orbital mechanics, Parabolic trajectory, Radial trajectory, Semi-major and semi-minor axes, Specific relative angular momentum.

Apsis

An apsis (ἁψίς; plural apsides, Greek: ἁψῖδες) is an extreme point in the orbit of an object.

Apsis and Elliptic orbit · Apsis and Kepler orbit · See more »

Asteroid

Asteroids are minor planets, especially those of the inner Solar System.

Asteroid and Elliptic orbit · Asteroid and Kepler orbit · See more »

Barycenter

The barycenter (or barycentre; from the Ancient Greek βαρύς heavy + κέντρον centre) is the center of mass of two or more bodies that are orbiting each other, which is the point around which they both orbit.

Barycenter and Elliptic orbit · Barycenter and Kepler orbit · See more »

Celestial mechanics

Celestial mechanics is the branch of astronomy that deals with the motions of celestial objects.

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Ellipse

In mathematics, an ellipse is a curve in a plane surrounding two focal points such that the sum of the distances to the two focal points is constant for every point on the curve.

Ellipse and Elliptic orbit · Ellipse and Kepler orbit · See more »

Gravitational two-body problem

←For further relevant mathematical developments see also Two-body problem, also Kepler orbit, and Kepler problem, and Equation of the center – Analytical expansions The gravitational two-body problem concerns the motion of two point particles that interact only with each other, due to gravity.

Elliptic orbit and Gravitational two-body problem · Gravitational two-body problem and Kepler orbit · See more »

Hyperbolic trajectory

In astrodynamics or celestial mechanics, a hyperbolic trajectory is the trajectory of any object around a central body with more than enough speed to escape the central object's gravitational pull.

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Isaac Newton

Sir Isaac Newton (25 December 1642 – 20 March 1726/27) was an English mathematician, astronomer, theologian, author and physicist (described in his own day as a "natural philosopher") who is widely recognised as one of the most influential scientists of all time, and a key figure in the scientific revolution.

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Johannes Kepler

Johannes Kepler (December 27, 1571 – November 15, 1630) was a German mathematician, astronomer, and astrologer.

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Kepler's laws of planetary motion

In astronomy, Kepler's laws of planetary motion are three scientific laws describing the motion of planets around the Sun.

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Newton's law of universal gravitation

Newton's law of universal gravitation states that a particle attracts every other particle in the universe with a force which is directly proportional to the product of their masses and inversely proportional to the square of the distance between their centers.

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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.

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Orbital elements

Orbital elements are the parameters required to uniquely identify a specific orbit.

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Orbital mechanics

Orbital mechanics or astrodynamics is the application of ballistics and celestial mechanics to the practical problems concerning the motion of rockets and other spacecraft.

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Parabolic trajectory

In astrodynamics or celestial mechanics a parabolic trajectory is a Kepler orbit with the eccentricity equal to 1.

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Radial trajectory

In astrodynamics and celestial mechanics a radial trajectory is a Kepler orbit with zero angular momentum.

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Semi-major and semi-minor axes

In geometry, the major axis of an ellipse is its longest diameter: a line segment that runs through the center and both foci, with ends at the widest points of the perimeter.

Elliptic orbit and Semi-major and semi-minor axes · Kepler orbit and Semi-major and semi-minor axes · See more »

Specific relative angular momentum

In celestial mechanics the specific relative angular momentum \vec plays a pivotal role in the analysis of the two-body problem.

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The list above answers the following questions

Elliptic orbit and Kepler orbit Comparison

Elliptic orbit has 49 relations, while Kepler orbit has 75. As they have in common 18, the Jaccard index is 14.52% = 18 / (49 + 75).

References

This article shows the relationship between Elliptic orbit and Kepler orbit. To access each article from which the information was extracted, please visit:

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