Difference between revisions of "Template:OrbitAltitude"

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m (!one opening bracket to many;)
m (!default is available as km/m;)
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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|}}}|&nbsp;{{#if: {{{radius_km|}}}|km|m}}}}</includeonly><noinclude>
+
<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}}}|&nbsp;{{{suffix|{{#if: {{{radius_km|}}}|km|m}}}}}}}</includeonly><noinclude>
  
 
{| class="wikitable"
 
{| class="wikitable"

Revision as of 19:47, 6 April 2013


Usage Produces
{{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).