Period charge

[symaski62]

http://en.wikibooks.org/wiki/Celestia/SSC_File

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For a closed, elliptical orbit around our Sun,

P = sqrt (( q / ( 1 - e)) ^3)
or = a^1.5

When defining an hyperbolic orbit around our Sun, set period to be

P = sqrt (( q / ( e - 1)) ^3)

CHARGE

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For a closed, elliptical orbit around our Sun,

P = ( q / ( 1 - e)) ^1,5

or = a^1.5

When defining an hyperbolic orbit around our Sun, set period to be

P = ( q / ( e - 1)) ^1,5