A library to make satellite propagation via TLEs possible in the web. Provides the functions necessary for SGP4/SDP4 calculations, as callable javascript. Also provides functions for coordinate transforms.
The internals of this library are nearly identical to Brandon Rhode's sgp4 python library. However, it is encapsulated in a standard JS library (self executing function), and exposes only the functionality needed to track satellites and propagate paths. The only changes I made to Brandon Rhode's code was to change the positional parameters of functions to key:value objects. This reduces the complexity of functions that require 50+ parameters, and doesn't require the parameters to be placed in the exact order.
Special thanks to all contributors for improving usability and bug fixes :)
If you want to contribute to the project please read the Contributing section first.
Sites using the library can be found here.
Start Here:
The javascript in this library is heavily based (straight copied) from:
I've included the original PKG-INFO file from the python library.
The coordinate transforms are based off T.S. Kelso's columns:
And the coursework for UC Boulder's ASEN students
I would recommend anybody interested in satellite tracking or orbital propagation to read all of TS Kelso's columns. Without his work, this project would not be possible.
Get a free Space Track account and download your own up to date TLEs for use with this library.
Install the library with NPM:
npm install satellite.js
Install the library with Yarn:
yarn add satellite.js
Install the library with Bower:
bower install satellite.js
Warning!
satellite.js
version 1.3.0 is the latest one for Bower since it has been deprecated.
var satellite = require('satellite.js');
...
var positionAndVelocity = satellite.sgp4(satrec, time);
import { sgp4 } from 'satellite.js';
...
const positionAndVelocity = sgp4(satrec, time);
define(['path/to/dist/satellite'], function(satellite) {
...
var positionAndVelocity = satellite.sgp4(satrec, time);
});
Here is a repo showing basic library usage with Require.js.
Include dist/satellite.min.js
as a script in your html:
<script src="https://github.com/shashwatak/satellite-js/raw/develop/path/to/dist/satellite.min.js"></script>
satellite
object will be available in global scope:
var positionAndVelocity = satellite.sgp4(satrec, time);
// Sample TLE
var tleLine1 = '1 25544U 98067A 19156.50900463 .00003075 00000-0 59442-4 0 9992',
tleLine2 = '2 25544 51.6433 59.2583 0008217 16.4489 347.6017 15.51174618173442';
// Initialize a satellite record
var satrec = satellite.twoline2satrec(tleLine1, tleLine2);
// Propagate satellite using time since epoch (in minutes).
var positionAndVelocity = satellite.sgp4(satrec, timeSinceTleEpochMinutes);
// Or you can use a JavaScript Date
var positionAndVelocity = satellite.propagate(satrec, new Date());
// The position_velocity result is a key-value pair of ECI coordinates.
// These are the base results from which all other coordinates are derived.
var positionEci = positionAndVelocity.position,
velocityEci = positionAndVelocity.velocity;
// Set the Observer at 122.03 West by 36.96 North, in RADIANS
var observerGd = {
longitude: satellite.degreesToRadians(-122.0308),
latitude: satellite.degreesToRadians(36.9613422),
height: 0.370
};
// You will need GMST for some of the coordinate transforms.
// http://en.wikipedia.org/wiki/Sidereal_time#Definition
var gmst = satellite.gstime(new Date());
// You can get ECF, Geodetic, Look Angles, and Doppler Factor.
var positionEcf = satellite.eciToEcf(positionEci, gmst),
observerEcf = satellite.geodeticToEcf(observerGd),
positionGd = satellite.eciToGeodetic(positionEci, gmst),
lookAngles = satellite.ecfToLookAngles(observerGd, positionEcf),
dopplerFactor = satellite.dopplerFactor(observerCoordsEcf, positionEcf, velocityEcf);
// The coordinates are all stored in key-value pairs.
// ECI and ECF are accessed by `x`, `y`, `z` properties.
var satelliteX = positionEci.x,
satelliteY = positionEci.y,
satelliteZ = positionEci.z;
// Look Angles may be accessed by `azimuth`, `elevation`, `range_sat` properties.
var azimuth = lookAngles.azimuth,
elevation = lookAngles.elevation,
rangeSat = lookAngles.rangeSat;
// Geodetic coords are accessed via `longitude`, `latitude`, `height`.
var longitude = positionGd.longitude,
latitude = positionGd.latitude,
height = positionGd.height;
// Convert the RADIANS to DEGREES.
var longitudeDeg = satellite.degreesLong(longitude),
latitudeDeg = satellite.degreesLat(latitude);
This repo follows Gitflow Workflow.
Before starting a work on new pull request, please, checkout your
feature or bugfix branch from develop
branch:
git checkout develop
git fetch origin
git merge origin/develop
git checkout -b my-feature
Make sure that your changes don't break the existing code by running
npm test
and that your code follows Airbnb style
npm run lint
npm run lint:test
Implementing new functions or features, please, if possible, provide tests to cover them and mention your works in
Changelog. Please don't change version number in package.json
and don't add it to CHANGELOG.md
.
All these things should be done later with raise-version when
merging to master
:
npm run raise major
or
npm run raise minor
or
npm run raise patch
In order to get test code coverage run the following:
npm run test:coverage
The source code is organized as Common.js modules and uses ES6 syntax.
In order to build the library follow these steps:
install Node.js and Node Package Manager;
install all required packages with NPM by running the following command from repository's root directory:
npm install
run the following NPM script to build everything:
npm run build
run the following NPM script to run test specs test/*.spec.js
files with Mocha:
npm test
These is a full list of all available NPM scripts:
build
builds everything;transpile
transpiles ES source files located in src
directory to Common.js compatible modules and saves
the resulting files in lib
directory;dist
builds ES and UMD modules in dist
directory;dist:es
builds ES module in dist
directory;dist:umd
builds UMD module in dist
directory (both non-compressed and
compressed versions);dist:umd:dev
builds non-compressed version of UMD module in dist
directory;dist:umd:prod
builds compressed version of UMD module in dist
directory; watch:es
watches for changes in src
directory and automatically rebuilds ES module;copy
copies built library from dist
to SGP4 verification application's directory;lint
lints sources code located in src
directory with ESLint with
Airbnb shared configuration;lint:test
lints tests located in test
directory with ESLint;test
runs tests;test:coverage
runs tests with Istanbul coverage summary;test:coveralls
runs tests with Istanbul coverage summary and aggregates the results by
Coveralls; in order to run it locally
COVERALLS_REPO_TOKEN
is required:
COVERALLS_REPO_TOKEN=<token> npm run test:coveralls
Some people are confused that they can't just download a single satellite.js or satellite.min.js file. That is because satellite.js is not written in plain old JavaScript (ES5) anymore but ported to latter JavaScript versions ES6+.
Only the "src" directory is included in the Git repository, "dist" and "lib" directories are ignored. It's done intentionally to retain the size of the repository as small as possible. A full detailed explanation of why is located here.
You should install satellite.js with your package manager (npm or yarn) and then find satellite.js and satellite.min.js in node_modules/satellite.js/dist directory.
Optional functions that utilize Worker Threads
The satrec
object comes from the original code by Rhodes as well as Vallado. It is immense and complex, but the
most important values it contains are the Keplerian Elements and the other values pulled from the TLEs. I do not
suggest that anybody try to simplify it unless they have absolute understanding of Orbital Mechanics.
satnum
Unique satellite number given in the TLE file.epochyr
Full four-digit year of this element set's epoch moment.epochdays
Fractional days into the year of the epoch moment.jdsatepoch
Julian date of the epoch (computed from epochyr
and epochdays
).ndot
First time derivative of the mean motion (ignored by SGP4).nddot
Second time derivative of the mean motion (ignored by SGP4).bstar
Ballistic drag coefficient B* in inverse earth radii.inclo
Inclination in radians.nodeo
Right ascension of ascending node in radians.ecco
Eccentricity.argpo
Argument of perigee in radians.mo
Mean anomaly in radians.no
Mean motion in radians per minute.var satrec = satellite.twoline2satrec(longstr1, longstr2);
returns satrec object, created from the TLEs passed in. The satrec object is vastly complicated, but you don't have to do anything with it, except pass it around.
NOTE! You are responsible for providing TLEs. Get your free Space Track account here. longstr1 and longstr2 are the two lines of the TLE, properly formatted by NASA and NORAD standards. if you use Space Track, there should be no problem.
Both propagate()
and sgp4()
functions return position and velocity as a dictionary of the form:
{
"position": { "x" : 1, "y" : 1, "z" : 1 },
"velocity": { "x" : 1, "y" : 1, "z" : 1 }
}
position is in km, velocity is in km/s, both the ECI coordinate frame.
var positionAndVelocity = satellite.propagate(satrec, new Date());
Returns position and velocity, given a satrec and the calendar date. Is merely a wrapper for sgp4()
, converts the
calendar day to Julian time since satellite epoch. Sometimes it's better to ask for position and velocity given
a specific date.
var positionAndVelocity = satellite.sgp4(satrec, timeSinceTleEpochMinutes);
Returns position and velocity, given a satrec and the time in minutes since epoch. Sometimes it's better to ask for position and velocity given the time elapsed since epoch.
You can get the satellites current Doppler factor, relative to your position, using the dopplerFactor()
function.
Use either ECI or ECF coordinates, but don't mix them.
var dopplerFactor = satellite.dopplerFactor(observer, position, velocity);
See the section on Coordinate Transforms to see how to get ECF/ECI/Geodetic coordinates.
You'll need to provide some of the coordinate transform functions with your current GMST aka GSTIME. You can use Julian Day:
var gmst = satellite.gstime(julianDay);
or a JavaScript Date:
var gmst = satellite.gstime(new Date());
Most of these are self explanatory from their names. Coords are arrays of three floats EX: [1.1, 1.2, 1.3] in kilometers. Once again, read the following first.
The coordinate transforms are based off T.S. Kelso's columns:
And the coursework for UC Boulder's ASEN students
These four are used to convert between ECI, ECF, and Geodetic, as you need them. ECI and ECF coordinates are in km or km/s. Geodetic coords are in radians.
var ecfCoords = satellite.eciToEcf(eciCoords, gmst);
var eciCoords = satellite.ecfToEci(ecfCoords, gmst);
var geodeticCoords = satellite.eciToGeodetic(eciCoords, gmst);
var ecfCoords = satellite.geodeticToEcf(geodeticCoords);
These function is used to compute the look angle, from your geodetic position to a satellite in ECF coordinates. Make sure you convert the ECI output from sgp4() and propagate() to ECF first.
var lookAngles = satellite.ecfToLookAngles(observerGeodetic, satelliteEcf);
These two functions will return human readable Latitude or Longitude strings (Ex: "125.35W" or "45.565N")
from geodeticCoords
:
var latitudeStr = satellite.degreesLat(geodeticRadians),
longitudeStr = satellite.degreesLong(geodeticRadians);
Like Brandon Rhodes before me, I chose to maintain as little difference between this implementation and the prior works. This is to make adapting future changes suggested by Vallado much simpler. Thus, some of the conventions used in this library are very weird.
I took advantage of the fact that Python and JavaScript are nearly semantically identical. Most of the code is just copied straight from Python. Brandon Rhodes did me the favor of including semi-colons on most of the lines of code. JavaScript doesn't support multiple values returned per statement, so I had to rewrite the function calls. Absolutely none of the mathematical logic had to be rewritten.
I've included a small testing app, that provides some benchmarking tools and verifies SGP4 and SDP4 using the Test Criteria provided by SpaceTrack Report #3, and is based off System Benchmarking by TS Kelso.
The testing app is a Chrome Packaged App that uses the angular.js
framework.
Before running the app build the library and copy resulting files from dist
directory to app's directory with
the following command:
npm run copy
To run the test, open up Chrome, go to the extensions page, and check "Developer Mode". Then, click "Load Unpacked App",
and select the sgp4_verification
folder. Then run the app from within Chrome. The test file is located within
the sgp4_verification
directory, as a JSON file called spacetrack-report-3.json
.
Major thanks go to Brandon Rhodes, TS Kelso, and David Vallado's team. Also, I'd like to thank Professor Steve Petersen (AC6P) of UCSC for pointing me in the correct directions.
All files marked with the License header at the top are Licensed. Any files unmarked by me or others are unlicensed, and are kept only as a resource for [Shashwat Kandadai and other developers] for testing.
I chose the MIT License because this library is a derivative work off Brandon Rhodes sgp4, and that is licensed with MIT. It just seemed simpler this way, sub-licensing freedoms notwithstanding.
I worked in the Dining Hall at UCSC for a month, which means I signed a form that gives UCSC partial ownership of anything I make while under their aegis, so I included them as owners of the copyright.
Please email all complaints to help@ucsc.edu