(Q2946193)

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Kepler orbit

describes the motion of an orbiting body as an ellipse, parabola, or hyperbola

Keplerian orbit

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r(\theta )={\frac {a(1-e^{2})}{1+e\cos(\theta )}}

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Keplerian elements

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WikiProject Mathematics

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different from

Keplerian elements

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Encyclopedia of China (Third Edition) ID

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28 October 2013

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Microsoft Academic ID

88599020

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Unified Astronomy Thesaurus ID

884

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(Q2946193)

Kepler orbit

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