fn main() {
let orbit = europas::physics::orbit::EuropaOrbit::new();
println!("Semi-major axis: {:.0} m", orbit.semi_major_axis_m);
println!(
"Orbital period: {:.2} days",
orbit.orbital_period_s() / 86_400.0
);
println!(
"Speed: {:.1} m/s",
orbit.orbital_speed_m_s(orbit.semi_major_axis_m)
);
let rot = europas::physics::rotation::EuropaRotation::new();
println!("Synchronous: {}", rot.synchronous);
println!("Equatorial speed: {:.2} m/s", rot.equatorial_speed_m_s());
}