package orbit;
public class Main {
public static void main(String[] args) {
String[] iss_2Line = {"1 25544U 98067A 03007.53073344 .00041100 00000-0 34010-3 0 9019",
"2 25544 51.6346 107.2569 0004536 6.6073 353.5141 15.58656572 35940"};
String[] sat_data = {"1 88888U 80275.98708465 .00073094 13844-3 66816-4 0 8 ",
"2 88888 72.8435 115.9689 0086731 52.6988 110.5714 16.05824518 105 "};
TwoLineElement tle = new TwoLineElement(iss_2Line);
Computations calc = new Computations(tle);
int delta = 360; double elapsedTime = 0;
for (int i = 0; i < 5; i++) {
calc.sgp4(elapsedTime, tle);
elapsedTime += delta;
}
}
}