orbital eccentricity (Q6387): Difference between revisions

Revision as of 19:35, 6 April 2023

parameter that determines the amount by which an orbit deviates from a perfect circle

Language	Label	Description	Also known as
English	orbital eccentricity	parameter that determines the amount by which an orbit deviates from a perfect circle	eccentricity

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e={\sqrt {1+{\frac {2EL^{2}}{m_{\text{red}}\alpha ^{2}}}}}

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Revision as of 19:34, 6 April 2023 Fire (talk \| contribs) Bureaucrats, Interface administrators, Administrators 132,454 edits ‎Created claim: part of (P7): Keplerian elements (Q6386) ← Older edit	Revision as of 19:35, 6 April 2023 Fire (talk \| contribs) Bureaucrats, Interface administrators, Administrators 132,454 edits ‎Created claim: defining formula (P333): e = \sqrt{1 + \frac{2 E L^2}{m_\text{red} \alpha ^2}} Newer edit →
	Property / defining formula
		$e={\sqrt {1+{\frac {2EL^{2}}{m_{\text{red}}\alpha ^{2}}}}}$ `e = \sqrt{1 + \frac{2 E L^2}{m_\text{red} \alpha ^2}}`
	Property / defining formula: $e={\sqrt {1+{\frac {2EL^{2}}{m_{\text{red}}\alpha ^{2}}}}}$ / rank
		Normal rank