File:Counterintuitive orbital mechanics.svg
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| Description |
At the top of the diagram by CMG Lee, a satellite in a clockwise circular orbit (yellow spot) launches objects of negligible mass: (1 - blue) towards Earth, (2 - red) away from Earth, (3 - grey) in the direction of travel, and (4 - black) backwards of the direction of travel. Dashed ellipses are orbits relative to Earth. Solid curves are pertubations relative to the satellite: in one orbit, (1) and (2) return to the satellite having made a clockwise loop on either side of the satellite. Unintuitively, (3) spirals farther and farther behind whereas (4) spirals ahead. |
| Source | Own work |
| Author | Cmglee |
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Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts. A copy of the license is included in the section entitled GNU Free Documentation License. |
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File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 01:29, 28 August 2021 | | 512 × 512 (25 KB) | Cmglee (talk | contribs) | Use SVG orb |
| 12:55, 3 February 2021 |  | 512 × 512 (24 KB) | Cmglee (talk | contribs) | Use currentColor and fix arrowheads. | |
| 02:23, 9 January 2021 |  | 512 × 512 (24 KB) | Cmglee (talk | contribs) | Increase launch speed and reduce number of "frames" to show orbits more clearly. | |
| 00:32, 15 December 2020 |  | 512 × 512 (32 KB) | Cmglee (talk | contribs) | {{Information |Description=At the top of the diagram by CMG Lee, a satellite in a clockwise circular orbit (yellow spot) launches objects of negligible mass:<br />(1 - blue) towards Earth,<br />(2 - red) away from Earth,<br />(3 - grey) in the direction of travel, and<br />(4 - black) backwards of the direction of travel.<br /><br />Dashed ellipses are orbits relative to Earth. Solid curves are pertubations relative to the satellite: in one orbit, (1) and (2) return to the satellite having ma... |
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