globe sizing
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ac3a890824
commit
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2 changed files with 394 additions and 392 deletions
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@ -1,335 +1,304 @@
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<div class="globeContainer">
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<svg id="globe" width="400" height="400"></svg>
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<div class="globeText">
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click and drag
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</div>
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</div>
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<style>
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.globeContainer {
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width: 100%;
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height: 100%;
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align-items: center;
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justify-content: center;
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background-color: #00111d;
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color: #ffffff;
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}
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:global(.footprint--LEO) {
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fill: rgba(255, 177, 64, 0.08);
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stroke: rgba(255, 177, 64, 0.5);
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}
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.globeText{
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text-align: center;
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font-size: 0.6em;
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color: #aaaaaa;
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}
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#globe {
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display: block;
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}
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</style>
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<script>
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import * as d3 from "d3";
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import * as sjs from 'satellite.js';
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import { onMount } from 'svelte';
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import tles from "../../static/tle.js"
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import world110m from "../../static/world-110m.js"
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import * as topojson from "topojson";
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export let width = 300;
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async function doThing() {
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let satelliteJs = sjs;
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var RADIANS = Math.PI / 180;
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var DEGREES = 180 / Math.PI;
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var R_EARTH = 6378.137; // equatorial radius (km)
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import * as d3 from "d3";
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import * as sjs from "satellite.js";
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import { onMount } from "svelte";
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import tles from "../../static/tle.js";
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import world110m from "../../static/world-110m.js";
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import * as topojson from "topojson";
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/* =============================================== */
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/* =============== CLOCK ========================= */
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/* =============================================== */
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export let width = 300;
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/**
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* Factory function for keeping track of elapsed time and rates.
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*/
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class Clock {
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constructor() {
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this._rate = 60; // 1ms elapsed : 60sec simulated
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this._date = d3.now();
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this._elapsed = 0;
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async function doThing() {
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let satelliteJs = sjs;
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var RADIANS = Math.PI / 180;
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var DEGREES = 180 / Math.PI;
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var R_EARTH = 6378.137; // equatorial radius (km)
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/* =============================================== */
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/* =============== CLOCK ========================= */
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/* =============================================== */
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/**
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* Factory function for keeping track of elapsed time and rates.
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*/
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class Clock {
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constructor() {
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this._rate = 60; // 1ms elapsed : 60sec simulated
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this._date = d3.now();
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this._elapsed = 0;
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}
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async date(timeInMs) {
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if (!arguments.length) return this._date + this._elapsed * this._rate;
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this._date = timeInMs;
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return this;
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}
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async elapsed(ms) {
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if (!arguments.length) return this._date - d3.now(); // calculates elapsed
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this._elapsed = ms;
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return this;
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}
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async rate(secondsPerMsElapsed) {
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if (!arguments.length) return this._rate;
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this._rate = secondsPerMsElapsed;
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return this;
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}
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}
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async date(timeInMs) {
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if (!arguments.length) return this._date + this._elapsed * this._rate;
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this._date = timeInMs;
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return this;
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}
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async elapsed(ms) {
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if (!arguments.length) return this._date - d3.now(); // calculates elapsed
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this._elapsed = ms;
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return this;
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}
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async rate(secondsPerMsElapsed) {
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if (!arguments.length) return this._rate;
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this._rate = secondsPerMsElapsed;
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return this;
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}
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}
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/* ==================================================== */
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/* =============== CONVERSION ========================= */
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/* ==================================================== */
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/* ==================================================== */
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/* =============== CONVERSION ========================= */
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/* ==================================================== */
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async function satrecToFeature(satrec, date, props) {
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var properties = props || {};
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var positionAndVelocity = satelliteJs.propagate(satrec, date);
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var gmst = satelliteJs.gstime(date);
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var positionGd = satelliteJs.eciToGeodetic(
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positionAndVelocity.position,
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gmst
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);
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properties.height = positionGd.height;
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return {
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type: "Feature",
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properties: properties,
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geometry: {
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type: "Point",
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coordinates: [
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positionGd.longitude * DEGREES,
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positionGd.latitude * DEGREES,
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],
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},
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};
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}
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/* ==================================================== */
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/* =============== TLE ================================ */
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/* ==================================================== */
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async function satrecToFeature(satrec, date, props) {
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var properties = props || {};
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var positionAndVelocity = satelliteJs.propagate(satrec, date);
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var gmst = satelliteJs.gstime(date);
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var positionGd = satelliteJs.eciToGeodetic(
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positionAndVelocity.position,
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gmst
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);
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properties.height = positionGd.height;
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return {
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type: "Feature",
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properties: properties,
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geometry: {
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type: "Point",
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coordinates: [
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positionGd.longitude * DEGREES,
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positionGd.latitude * DEGREES,
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],
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},
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};
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}
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/* ==================================================== */
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/* =============== TLE ================================ */
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/* ==================================================== */
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/**
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* Factory function for working with TLE.
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*/
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class TLE {
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constructor() {
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this._properties;
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/**
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* Factory function for working with TLE.
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*/
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class TLE {
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constructor() {
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this._properties;
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this._date;
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}
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async _lines(arry) {
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return arry.slice(0, 2);
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}
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async satrecs(tles) {
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return tles.map(function (d) {
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return satelliteJs.twoline2satrec.apply(null, this._lines(d));
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});
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}
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async features(tles) {
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var date = this._date || d3.now();
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return tles.map(function (d) {
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var satrec = satelliteJs.twoline2satrec.apply(null, this._lines(d));
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return satrecToFeature(satrec, date, this._properties(d));
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});
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}
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async lines(func) {
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if (!arguments.length) return this._lines;
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this._lines = func;
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return this;
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}
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async properties(func) {
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if (!arguments.length) return this._properties;
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this._properties = func;
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return this;
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}
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async date(ms) {
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if (!arguments.length) return this._date;
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this._date = ms;
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return this;
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}
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}
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/* ==================================================== */
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/* =============== PARSE ============================== */
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/* ==================================================== */
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/**
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* Parses text file string of tle into groups.
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* @return {string[][]} Like [['tle line 1', 'tle line 2'], ...]
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*/
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async function parseTle(tleString) {
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// remove last newline so that we can properly split all the lines
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var lines = tleString.replace(/\r?\n$/g, "").split(/\r?\n/);
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return lines.reduce(function (acc, cur, index) {
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if (index % 2 === 0) acc.push([]);
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acc[acc.length - 1].push(cur);
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return acc;
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}, []);
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}
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/* ==================================================== */
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/* =============== SATELLITE ========================== */
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/* ==================================================== */
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/**
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* Satellite factory function that wraps satellitejs functionality
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* and can compute footprints based on TLE and date
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*
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* @param {string[][]} tle two-line element
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* @param {Date} date date to propagate with TLE
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*/
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function Satellite(tle, date) {
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this._satrec = satelliteJs.twoline2satrec(tle[0], tle[1]);
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this._satNum = this._satrec.satnum; // NORAD Catalog Number
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this._altitude; // km
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this._position = {
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lat: null,
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lng: null,
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};
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this._halfAngle; // degrees
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this._date;
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}
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async _lines(arry) {
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return arry.slice(0, 2);
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}
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async satrecs(tles) {
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return tles.map(function (d) {
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return satelliteJs.twoline2satrec.apply(null, this._lines(d));
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});
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}
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async features(tles) {
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var date = this._date || d3.now();
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this._gmst;
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return tles.map(function (d) {
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var satrec = satelliteJs.twoline2satrec.apply(null, this._lines(d));
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return satrecToFeature(satrec, date, this._properties(d));
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});
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this.setDate(date);
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this.update();
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this._orbitType = this.orbitTypeFromAlt(this._altitude); // LEO, MEO, or GEO
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}
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async lines(func) {
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if (!arguments.length) return this._lines;
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this._lines = func;
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/**
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* Updates satellite position and altitude based on current TLE and date
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*/
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Satellite.prototype.update = async function () {
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var positionAndVelocity = satelliteJs.propagate(this._satrec, this._date);
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var positionGd = satelliteJs.eciToGeodetic(
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positionAndVelocity.position,
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this._gmst
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);
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this._position = {
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lat: positionGd.latitude * DEGREES,
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lng: positionGd.longitude * DEGREES,
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};
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this._altitude = positionGd.height;
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return this;
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}
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async properties(func) {
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if (!arguments.length) return this._properties;
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this._properties = func;
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return this;
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}
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async date(ms) {
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if (!arguments.length) return this._date;
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this._date = ms;
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return this;
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}
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}
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/* ==================================================== */
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/* =============== PARSE ============================== */
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/* ==================================================== */
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/**
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* Parses text file string of tle into groups.
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* @return {string[][]} Like [['tle line 1', 'tle line 2'], ...]
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*/
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async function parseTle(tleString) {
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// remove last newline so that we can properly split all the lines
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var lines = tleString.replace(/\r?\n$/g, "").split(/\r?\n/);
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return lines.reduce(function (acc, cur, index) {
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if (index % 2 === 0) acc.push([]);
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acc[acc.length - 1].push(cur);
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return acc;
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}, []);
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}
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/* ==================================================== */
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/* =============== SATELLITE ========================== */
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/* ==================================================== */
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/**
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* Satellite factory function that wraps satellitejs functionality
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* and can compute footprints based on TLE and date
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*
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* @param {string[][]} tle two-line element
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* @param {Date} date date to propagate with TLE
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*/
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function Satellite(tle, date) {
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this._satrec = satelliteJs.twoline2satrec(tle[0], tle[1]);
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this._satNum = this._satrec.satnum; // NORAD Catalog Number
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this._altitude; // km
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this._position = {
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lat: null,
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lng: null,
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};
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this._halfAngle; // degrees
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this._date;
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this._gmst;
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this.setDate(date);
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this.update();
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this._orbitType = this.orbitTypeFromAlt(this._altitude); // LEO, MEO, or GEO
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}
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/**
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* @returns {GeoJSON.Polygon} GeoJSON describing the satellite's current footprint on the Earth
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*/
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Satellite.prototype.getFootprint = function () {
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var theta = this._halfAngle * RADIANS;
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/**
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* Updates satellite position and altitude based on current TLE and date
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*/
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Satellite.prototype.update = async function () {
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var positionAndVelocity = satelliteJs.propagate(this._satrec, this._date);
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var positionGd = satelliteJs.eciToGeodetic(
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positionAndVelocity.position,
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this._gmst
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);
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let coreAngle = this._coreAngle(theta, this._altitude, R_EARTH) * DEGREES;
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this._position = {
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lat: positionGd.latitude * DEGREES,
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lng: positionGd.longitude * DEGREES,
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return d3
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.geoCircle()
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.center([this._position.lng, this._position.lat])
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.radius(coreAngle)();
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};
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this._altitude = positionGd.height;
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return this;
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};
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/**
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* @returns {GeoJSON.Polygon} GeoJSON describing the satellite's current footprint on the Earth
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*/
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Satellite.prototype.getFootprint = function () {
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var theta = this._halfAngle * RADIANS;
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/**
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* A conical satellite with half angle casts a circle on the Earth. Find the angle
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* from the center of the earth to the radius of this circle
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* @param {number} theta: Satellite half angle in radians
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* @param {number} altitude Satellite altitude
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* @param {number} r Earth radius
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* @returns {number} core angle in radians
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*/
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Satellite.prototype._coreAngle = function (theta, altitude, r) {
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// if FOV is larger than Earth, assume it goes to the tangential point
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if (Math.sin(theta) > r / (altitude + r)) {
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return Math.acos(r / (r + altitude));
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}
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return (
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Math.abs(Math.asin(((r + altitude) * Math.sin(theta)) / r)) - theta
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);
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};
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let coreAngle = this._coreAngle(theta, this._altitude, R_EARTH) * DEGREES;
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Satellite.prototype.halfAngle = function (halfAngle) {
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if (!arguments.length) return this._halfAngle;
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this._halfAngle = halfAngle;
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return this;
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};
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return d3
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.geoCircle()
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.center([this._position.lng, this._position.lat])
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.radius(coreAngle)();
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};
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Satellite.prototype.satNum = function (satNum) {
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if (!arguments.length) return this._satNum;
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this._satNum = satNum;
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return this;
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};
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/**
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* A conical satellite with half angle casts a circle on the Earth. Find the angle
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* from the center of the earth to the radius of this circle
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* @param {number} theta: Satellite half angle in radians
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* @param {number} altitude Satellite altitude
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* @param {number} r Earth radius
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* @returns {number} core angle in radians
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*/
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Satellite.prototype._coreAngle = function (theta, altitude, r) {
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// if FOV is larger than Earth, assume it goes to the tangential point
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if (Math.sin(theta) > r / (altitude + r)) {
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return Math.acos(r / (r + altitude));
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}
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return Math.abs(Math.asin(((r + altitude) * Math.sin(theta)) / r)) - theta;
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};
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Satellite.prototype.altitude = function (altitude) {
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if (!arguments.length) return this._altitude;
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this._altitude = altitude;
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return this;
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};
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Satellite.prototype.halfAngle = function (halfAngle) {
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if (!arguments.length) return this._halfAngle;
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this._halfAngle = halfAngle;
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return this;
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};
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Satellite.prototype.position = function (position) {
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if (!arguments.length) return this._position;
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this._position = position;
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return this;
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};
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Satellite.prototype.satNum = function (satNum) {
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if (!arguments.length) return this._satNum;
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this._satNum = satNum;
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return this;
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};
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Satellite.prototype.getOrbitType = function () {
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return this._orbitType;
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};
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Satellite.prototype.altitude = function (altitude) {
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if (!arguments.length) return this._altitude;
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this._altitude = altitude;
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return this;
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};
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/**
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* sets both the date and the Greenwich Mean Sidereal Time
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* @param {Date} date
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*/
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Satellite.prototype.setDate = function (date) {
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this._date = date;
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this._gmst = satelliteJs.gstime(date);
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return this;
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};
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Satellite.prototype.position = function (position) {
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if (!arguments.length) return this._position;
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this._position = position;
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return this;
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};
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/**
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* Maps an altitude to a type of satellite
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* @param {number} altitude (in KM)
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* @returns {'LEO' | 'MEO' | 'GEO'}
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*/
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Satellite.prototype.orbitTypeFromAlt = function (altitude) {
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this._altitude = altitude || this._altitude;
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return this._altitude < 1200
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? "LEO"
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: this._altitude > 22000
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? "GEO"
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: "MEO";
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};
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Satellite.prototype.getOrbitType = function () {
|
||||
return this._orbitType;
|
||||
};
|
||||
/* =============================================== */
|
||||
/* =================== GLOBE ===================== */
|
||||
/* =============================================== */
|
||||
|
||||
/**
|
||||
* sets both the date and the Greenwich Mean Sidereal Time
|
||||
* @param {Date} date
|
||||
*/
|
||||
Satellite.prototype.setDate = function (date) {
|
||||
this._date = date;
|
||||
this._gmst = satelliteJs.gstime(date);
|
||||
return this;
|
||||
};
|
||||
// Approximate date the tle data was aquired from https://www.space-track.org/#recent
|
||||
var TLE_DATA_DATE = new Date(2015, 11, 3, 17, 36).getTime();
|
||||
|
||||
/**
|
||||
* Maps an altitude to a type of satellite
|
||||
* @param {number} altitude (in KM)
|
||||
* @returns {'LEO' | 'MEO' | 'GEO'}
|
||||
*/
|
||||
Satellite.prototype.orbitTypeFromAlt = function (altitude) {
|
||||
this._altitude = altitude || this._altitude;
|
||||
return this._altitude < 1200
|
||||
? "LEO"
|
||||
: this._altitude > 22000
|
||||
? "GEO"
|
||||
: "MEO";
|
||||
};
|
||||
var activeClock;
|
||||
var sats;
|
||||
|
||||
/* =============================================== */
|
||||
/* =================== GLOBE ===================== */
|
||||
/* =============================================== */
|
||||
var svg = d3.select("#globe");
|
||||
|
||||
// Approximate date the tle data was aquired from https://www.space-track.org/#recent
|
||||
var TLE_DATA_DATE = new Date(2015, 11, 3, 17 ,36).getTime();
|
||||
var marginTop = 0;
|
||||
var width = svg.attr("width");
|
||||
var height = svg.attr("height") - marginTop;
|
||||
|
||||
var activeClock;
|
||||
var sats;
|
||||
var projection = d3
|
||||
.geoOrthographic()
|
||||
.scale((height - 10) / 2)
|
||||
.translate([width / 2, height / 2 + marginTop])
|
||||
.rotate([45, -30]);
|
||||
|
||||
var svg = d3.select("#globe");
|
||||
var geoPath = d3.geoPath().projection(projection);
|
||||
|
||||
var marginTop = 0;
|
||||
var width = svg.attr("width");
|
||||
var height = svg.attr("height") - marginTop;
|
||||
svg
|
||||
.append("path")
|
||||
.datum({
|
||||
type: "Sphere",
|
||||
})
|
||||
.style("cursor", "grab")
|
||||
.attr("fill", "#2E86AB")
|
||||
.attr("d", geoPath);
|
||||
|
||||
var projection = d3
|
||||
.geoOrthographic()
|
||||
.scale((height - 10) / 2)
|
||||
.translate([width / 2, height / 2 + marginTop])
|
||||
.rotate([45, -30]);
|
||||
|
||||
var geoPath = d3.geoPath().projection(projection);
|
||||
|
||||
svg
|
||||
.append("path")
|
||||
.datum({
|
||||
type: "Sphere",
|
||||
})
|
||||
.style("cursor", "grab")
|
||||
.attr("fill", "#2E86AB")
|
||||
.attr("d", geoPath);
|
||||
|
||||
function initGlobe() {
|
||||
let worldData = world110m;
|
||||
function initGlobe() {
|
||||
let worldData = world110m;
|
||||
svg
|
||||
.selectAll(".segment")
|
||||
.data([topojson.feature(worldData, worldData.objects.land)])
|
||||
|
@ -342,111 +311,144 @@
|
|||
.style("stroke-width", "0px")
|
||||
.style("fill", "#ffffff")
|
||||
.style("opacity", "1");
|
||||
}
|
||||
}
|
||||
|
||||
async function updateSats(date) {
|
||||
sats.forEach(async function (sat) {
|
||||
return sat.setDate(date).update();
|
||||
});
|
||||
return sats;
|
||||
}
|
||||
async function updateSats(date) {
|
||||
sats.forEach(async function (sat) {
|
||||
return sat.setDate(date).update();
|
||||
});
|
||||
return sats;
|
||||
}
|
||||
|
||||
/**
|
||||
* Create satellite objects for each record in the TLEs and begin animation
|
||||
* @param {string[][]} parsedTles
|
||||
*/
|
||||
async function initSats(parsedTles) {
|
||||
activeClock = new Clock();
|
||||
/**
|
||||
* Create satellite objects for each record in the TLEs and begin animation
|
||||
* @param {string[][]} parsedTles
|
||||
*/
|
||||
async function initSats(parsedTles) {
|
||||
activeClock = new Clock();
|
||||
|
||||
await activeClock.rate(100);
|
||||
await activeClock.date(TLE_DATA_DATE);
|
||||
await activeClock.rate(100);
|
||||
await activeClock.date(TLE_DATA_DATE);
|
||||
|
||||
sats = await Promise.all(
|
||||
parsedTles.map(async function (tle) {
|
||||
var sat = new Satellite(tle, new Date(2015, 11, 3, 17, 36));
|
||||
sat.halfAngle(61.73);
|
||||
return sat;
|
||||
})
|
||||
);
|
||||
|
||||
window.requestAnimationFrame(animateSats);
|
||||
return sats;
|
||||
}
|
||||
|
||||
async function draw() {
|
||||
// redrawGlobe();
|
||||
let allFootprints = svg.selectAll(".footprint");
|
||||
|
||||
let allFootprintsData = allFootprints.data(sats, async function (sat) {
|
||||
return sat.satNum();
|
||||
});
|
||||
|
||||
let allFootprintsDataJoin = allFootprintsData.join(function (enter) {
|
||||
return enter
|
||||
.append("path")
|
||||
.attr("class", function (sat) {
|
||||
return "footprint footprint--" + sat.getOrbitType();
|
||||
sats = await Promise.all(
|
||||
parsedTles.map(async function (tle) {
|
||||
var sat = new Satellite(tle, new Date(2015, 11, 3, 17, 36));
|
||||
sat.halfAngle(61.73);
|
||||
return sat;
|
||||
})
|
||||
.style("cursor", "grab");
|
||||
});
|
||||
);
|
||||
|
||||
allFootprintsDataJoin.attr("d", function (sat) {
|
||||
return geoPath(sat.getFootprint());
|
||||
});
|
||||
}
|
||||
|
||||
async function redrawGlobe() {
|
||||
let allSelectedSegment = svg.selectAll(".segment");
|
||||
allSelectedSegment.attr("d", geoPath);
|
||||
}
|
||||
|
||||
var m0;
|
||||
var o0;
|
||||
|
||||
async function mousedown(e) {
|
||||
m0 = [e.pageX, e.pageY];
|
||||
o0 = projection.rotate();
|
||||
e.preventDefault();
|
||||
}
|
||||
|
||||
async function mousemove(e) {
|
||||
if (m0) {
|
||||
var m1 = [e.pageX, e.pageY];
|
||||
const o1 = [o0[0] + (m1[0] - m0[0]) / 2.5, o0[1] + (m0[1] - m1[1]) / 2.5];
|
||||
projection.rotate(o1);
|
||||
redrawGlobe();
|
||||
window.requestAnimationFrame(animateSats);
|
||||
return sats;
|
||||
}
|
||||
}
|
||||
|
||||
async function mouseup(e) {
|
||||
if (m0) {
|
||||
mousemove(e);
|
||||
m0 = null;
|
||||
async function draw() {
|
||||
// redrawGlobe();
|
||||
let allFootprints = svg.selectAll(".footprint");
|
||||
|
||||
let allFootprintsData = allFootprints.data(sats, async function (sat) {
|
||||
return sat.satNum();
|
||||
});
|
||||
|
||||
let allFootprintsDataJoin = allFootprintsData.join(function (enter) {
|
||||
return enter
|
||||
.append("path")
|
||||
.attr("class", function (sat) {
|
||||
return "footprint footprint--" + sat.getOrbitType();
|
||||
})
|
||||
.style("cursor", "grab");
|
||||
});
|
||||
|
||||
allFootprintsDataJoin.attr("d", function (sat) {
|
||||
return geoPath(sat.getFootprint());
|
||||
});
|
||||
}
|
||||
|
||||
async function redrawGlobe() {
|
||||
let allSelectedSegment = svg.selectAll(".segment");
|
||||
allSelectedSegment.attr("d", geoPath);
|
||||
}
|
||||
|
||||
var m0;
|
||||
var o0;
|
||||
|
||||
async function mousedown(e) {
|
||||
m0 = [e.pageX, e.pageY];
|
||||
o0 = projection.rotate();
|
||||
e.preventDefault();
|
||||
}
|
||||
|
||||
async function mousemove(e) {
|
||||
if (m0) {
|
||||
var m1 = [e.pageX, e.pageY];
|
||||
const o1 = [
|
||||
o0[0] + (m1[0] - m0[0]) / 2.5,
|
||||
o0[1] + (m0[1] - m1[1]) / 2.5,
|
||||
];
|
||||
projection.rotate(o1);
|
||||
redrawGlobe();
|
||||
}
|
||||
}
|
||||
|
||||
async function mouseup(e) {
|
||||
if (m0) {
|
||||
mousemove(e);
|
||||
m0 = null;
|
||||
}
|
||||
}
|
||||
|
||||
svg.on("mousedown", mousedown);
|
||||
d3.select(window).on("mousemove", mousemove).on("mouseup", mouseup);
|
||||
|
||||
async function animateSats(elapsed) {
|
||||
var dateInMsI1 = await activeClock.elapsed(elapsed);
|
||||
var dateInMs = dateInMsI1.date();
|
||||
var date = new Date(await dateInMs);
|
||||
|
||||
updateSats(date);
|
||||
draw();
|
||||
window.requestAnimationFrame(animateSats);
|
||||
}
|
||||
|
||||
initGlobe();
|
||||
|
||||
await initSats(await parseTle(tles));
|
||||
}
|
||||
|
||||
svg.on("mousedown", mousedown);
|
||||
d3.select(window).on("mousemove", mousemove).on("mouseup", mouseup);
|
||||
onMount(async () => {
|
||||
doThing();
|
||||
});
|
||||
</script>
|
||||
|
||||
async function animateSats(elapsed) {
|
||||
var dateInMsI1 = await activeClock.elapsed(elapsed);
|
||||
var dateInMs = dateInMsI1.date();
|
||||
var date = new Date(await dateInMs);
|
||||
<div class="globeContainer">
|
||||
<svg id="globe" {width} height={width} />
|
||||
<div class="globeText">click and drag</div>
|
||||
</div>
|
||||
|
||||
updateSats(date);
|
||||
draw();
|
||||
window.requestAnimationFrame(animateSats);
|
||||
<style>
|
||||
.globeContainer {
|
||||
width: 100%;
|
||||
height: 100%;
|
||||
display: flex;
|
||||
align-items: center;
|
||||
justify-content: center;
|
||||
flex-direction: column;
|
||||
background-color: #00111d;
|
||||
color: #ffffff;
|
||||
}
|
||||
|
||||
initGlobe();
|
||||
|
||||
await initSats(await parseTle(tles))
|
||||
:global(.footprint--LEO) {
|
||||
fill: rgba(255, 177, 64, 0.08);
|
||||
stroke: rgba(255, 177, 64, 0.5);
|
||||
}
|
||||
|
||||
|
||||
|
||||
onMount(async () => {
|
||||
doThing();
|
||||
});
|
||||
|
||||
</script>
|
||||
.globeText {
|
||||
text-align: center;
|
||||
font-size: 0.6em;
|
||||
color: #aaaaaa;
|
||||
}
|
||||
|
||||
#globe {
|
||||
display: block;
|
||||
}
|
||||
</style>
|
||||
|
|
|
@ -15,7 +15,7 @@
|
|||
<div class="site">
|
||||
<div class="hero">
|
||||
<div class="container">
|
||||
<Globe />
|
||||
<Globe width="250" />
|
||||
<FemtoHeader />
|
||||
</div>
|
||||
</div>
|
||||
|
@ -105,7 +105,7 @@
|
|||
|
||||
.hero .container {
|
||||
grid-template-columns: auto;
|
||||
grid-template-rows: 200px auto;
|
||||
grid-template-rows: 260px auto;
|
||||
}
|
||||
}
|
||||
</style>
|
||||
|
|
Loading…
Reference in a new issue