Difference between revisions of "Template:OrbitAltitude"
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− | {{ | + | <includeonly>{{formatnum|{{#expr:((({{{period_s}}}^2 * {{G}} * {{{mass_kg}}}/(4 * pi^2)) ^ (1/3)) {{#if: {{{radius_km|}}}|*1000}} - {{#if: {{{radius_km|}}}|{{{radius_km}}}|{{{radius_m}}}}}}}|2}}{{#if: {{{suffix|}}}| {{#if: {{{radius_km|}}}|km|m}}}}</includeonly><noinclude> |
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− | This template calculates the altitude of an orbit, given the mass of the planet (in kg), the planet's radius (in km), and the period of the orbit (in seconds). | + | This template calculates the altitude of an orbit, given the mass of the planet (in kg), the planet's radius (in km or m), and the period of the orbit (in seconds). |
− | [[Category:Templates|OrbitAltitude]] | + | [[Category:Templates|OrbitAltitude]]</noinclude> |
− | </noinclude> |
Revision as of 19:38, 6 April 2013
Usage | Produces |
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{{OrbitAltitude | period_s=64980 | mass_kg=4.515e21 | radius_km=320}} |
0.00 m |
{{OrbitAltitude | period_s=64980 | mass_kg=4.515e21 | radius_m=320000}} |
0.00 m |
This template calculates the altitude of an orbit, given the mass of the planet (in kg), the planet's radius (in km or m), and the period of the orbit (in seconds).