TLE.go


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/*
Implementing the "Two-line element set (TLE)", a data format encoding orbital elements of Earth-orbiting objects. https://en.wikipedia.org/wiki/Two-line_element_set
*/

package TLE

// tlebytes defines a tle using raw bytes.
type TLE struct {
	TitleLine struct {
		Satname string `json:"satname"`
	} `json:"titleline"`
	LineOne struct {
		Linenumber              int8 `json:"linenumber"`
		Satellitenumber         int  `json:"satellitenumber"`
		Classification          rune `json:"classification"`
		InternationalDesignator struct {
			launchyear   int8 `json:"launchyear"`
			launchnumber int  `json:"launchnumber"`
			launchpiece  rune `json:"launchpiece"`
		} `json:"internationaldesignator"`
		Epoch struct {
			year        int8    `json:"year"`
			dayfraction float64 `json:"dayfraction"`
		}
		Firstderiv       float64 `json:"firstderiv"`
		Secondderiv      float64 `json:"secondderiv"`
		BSTAR            float64 `json:"BSTAR"`
		Numberzero       int8    `json:"numberzero"`
		ElementSetNumber int     `json:"elementesetnumber"`
		Checksum         int8    `json:"checksum"`
	} `json:"lineone"`
	LineTwo struct {
		Linenumber                       int8    `json:"linenumber"`
		Satellitenumber                  int     `json:"satellitenumber"`
		Inclination                      float64 `json:"inclination"`
		RightAscensionOfTheAscendingNode float64 `json:"rightascensionoftheascendingnode"`
		Eccentricity                     float64 `json:"eccentricity"`
		ArgumentOfPerigee                float64 `json:"argumentofperigee"`
		MeanAnomaly                      float64 `json:"meananomaly"`
		MeanMotion                       float64 `json:"meanmotion"`
		RevolutionNumberAtEpoch          int     `json:"revolutionnumberatepoch"`
		Checksum                         int8    `json:"checksum"`
	} `json:"linetwo"`
}