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tle.js
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tle.js
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import * as satellite from 'satellite.js/lib/index';
export const EarthRadius = 6371;
const rad2Deg = 180 / 3.141592654;
export const parseTleFile = (fileContent, stationOptions) => {
const result = [];
const lines = fileContent.split("\n");
let current = null;
for (let i = 0; i < lines.length; ++i) {
const line = lines[i].trim();
if (line.length === 0) continue;
if (line[0] === '1') {
current.tle1 = line;
}
else if (line[0] === '2') {
current.tle2 = line;
}
else {
current = {
name: line,
...stationOptions
};
result.push(current);
}
}
return result;
}
// __ Satellite locations _________________________________________________
const latLon2Xyz = (radius, lat, lon) => {
var phi = (90-lat)*(Math.PI/180)
var theta = (lon+180)*(Math.PI/180)
const x = -((radius) * Math.sin(phi) * Math.cos(theta))
const z = ((radius) * Math.sin(phi) * Math.sin(theta))
const y = ((radius) * Math.cos(phi))
return { x, y, z };
}
const toThree = (v) => {
return { x: v.x, y: v.z, z: -v.y };
}
const getSolution = (station, date) => {
if (!station.satrec) {
const { tle1, tle2 } = station;
if (!tle1 || !tle2) return null;
station.satrec = satellite.twoline2satrec(tle1, tle2);;
}
return satellite.propagate(station.satrec, date);
}
// type: 1 ECEF coordinates 2: ECI coordinates
export const getPositionFromTle = (station, date, type = 1) => {
if (!station || !date) return null;
const positionVelocity = getSolution(station, date);
const positionEci = positionVelocity.position;
if (type === 2) return [toThree(positionEci), positionEci];
const gmst = satellite.gstime(date);
if (!positionEci) return null; // Ignore
const positionEcf = satellite.eciToEcf(positionEci, gmst);
return [toThree(positionEcf), positionEci];
}
export const getPositionFromGroundCoords = (lat, long, height) => {
var observerGd = {
longitude: satellite.degreesToRadians(long),
latitude: satellite.degreesToRadians(lat),
height: height
}
const pos = satellite.geodeticToEcf(observerGd)
return [toThree(pos), observerGd];
}