def apply(self, satellite: Satellite) -> ManeuverCost:
orbit = satellite.orbit
cur_theta = satellite.true_anomaly()
new_theta = cur_theta + self.delta_theta
# Find the difference in s and wait by that much
cur_s = satellite.true_to_universal_anomaly(cur_theta)
new_s = satellite.true_to_universal_anomaly(new_theta)
delta_s = new_s - cur_s
satellite.wait_s(delta_s)
return ManeuverCost(delta_t=satellite.delta_s_to_t(delta_s))
