A small library to calculate satellite orbits from two-line elements.
import TLE from './TLE';
import Satellite from './Satellite';
const tle = new TLE("NOAA 14", "1 23455U 94089A 97320.90946019 .00000140 00000-0 10191-3 0 2621", "2 23455 99.0090 272.6745 0008546 223.1686 136.8816 14.11711747148495");
const sat = new Satellite(tle, 0.25);
- Orbits.js By rossengeorgiev
- Models for Propagation of NORAD Element Sets By Felix R. Hoots and Ronald L. Roehrichm, December 1980
- Orbital Coordinate Systems, Part III By Dr. T.S. Kelso