Difference between revisions of "Template:OrbitAltitude/Core"
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m (*replace 'Parameter Row' and 'ParameterRow' by 'Parameter row';) |
m (*renamed Parameter Table to Parameter table;) |
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|G=/1000000000}}}}</includeonly><noinclude>Calculates the orbital height without any formatting. | |G=/1000000000}}}}</includeonly><noinclude>Calculates the orbital height without any formatting. | ||
− | {{Parameter | + | {{Parameter table|parameters= |
{{Parameter row|1|Period of the orbit in seconds}} | {{Parameter row|1|Period of the orbit in seconds}} | ||
{{Parameter row|2|Mass of central body in kilograms}} | {{Parameter row|2|Mass of central body in kilograms}} |
Revision as of 12:12, 19 December 2014
Calculates the orbital height without any formatting.
# | Optional | Description | Default |
---|---|---|---|
1 | No | Period of the orbit in seconds | |
2 | No | Mass of central body in kilograms | |
3 | Yes | Radius of central body in meters | 0 |
f | Yes | Factor in which the altitude should be shown. Available values: None (m), k (km), M (Mm), G (Gm). If the radius was given kilometers it uses the factor k. | None |
b | Yes | Uses the sidereal rotation period, mass and radius as default from the given body. Can be overwritten. | Not set (makes the first three parameters mandatory) |
pf | Yes | Multiplies the period with this value. Useful to easily calculate semi-synchronous orbits (pf=1/2 then). | 1 |