[![GoDoc](https://godoc.org/git.darknebu.la/Satellite/TLE?status.svg)](https://godoc.org/git.darknebu.la/Satellite/TLE) [![Go Report Card](https://goreportcard.com/badge/git.darknebu.la/Satellite/TLE)](https://goreportcard.com/report/git.darknebu.la/Satellite/TLE) [![Build Status](https://drone.nbg1.emile.space/api/badges/Satellite/TLE/status.svg)](https://drone.nbg1.emile.space/Satellite/TLE) # TLE 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 [nasa documentation of the format](https://spaceflight.nasa.gov/realdata/sightings/SSapplications/Post/JavaSSOP/SSOP_Help/tle_def.html) ## Format (the below tables are copied 1:1 from wikipedia ([from here](https://en.wikipedia.org/wiki/Two-line_element_set))) ### Title line | Field | Columns | Content | Example | | ----- | ------- | ------- | ------- | | 1 | 01-24 | Satellite name | ISS (ZARYA) | ### Line one | Field | Columns | Content | Example | | ----- | ------- | ------- | ------- | | 1 | 01-01 | Line number | `1` | | 2 | 03–07 | Satellite number | `25544` | | 3 | 08–08 | Classification (U=Unclassified) | `U` | | 4 | 10–11 | International Designator (Last two digits of launch year) | `98` | | 5 | 12–14 | International Designator (Launch number of the year) | `067` | | 6 | 15–17 | International Designator (piece of the launch) | `A` | | 7 | 19–20 | Epoch Year (last two digits of year) | `08` | | 8 | 21–32 | Epoch (day of the year and fractional portion of the day) | `264.51782528` | | 9 | 34–43 | First Time Derivative of the Mean Motion divided by two [11] | `−.00002182` | | 10 | 45–52 | Second Time Derivative of Mean Motion divided by six (decimal point assumed) | `00000-0` | | 11 | 54–61 | BSTAR drag term (decimal point assumed) [11] | `-11606-4` | | 12 | 63–63 | The number 0 (originally this should have been "Ephemeris type") | `0` | | 13 | 65–68 | Element set number. Incremented when a new TLE is generated for this object.[11] | `292` | | 14 | 69–69 | Checksum (modulo 10) | `7`| ### Line two | Field | Columns | Content | Example | | ----- | ------- | ------- | ------- | | 1 | 01–01 | Line number | `2` | | 2 | 03–07 | Satellite number | `25544` | | 3 | 09–16 | Inclination (degrees) | `51.6416` | | 4 | 18–25 | Right ascension of the ascending node (degrees) | `247.4627` | | 5 | 27–33 | Eccentricity (decimal point assumed) | `0006703` | | 6 | 35–42 | Argument of perigee (degrees) | `130.5360` | | 7 | 44–51 | Mean Anomaly (degrees) | `325.0288` | | 8 | 53–63 | Mean Motion (revolutions per day) | `15.72125391` | | 9 | 64–68 | Revolution number at epoch (revolutions) | `56353` | | 10 | 69–69 | Checksum (modulo 10) | `7` |