public static void SetOrbit(string body, double semiMajorAxis, double eccentricity, double inclination, double longitudeOfAscendingNode, double argumentOfPeriapsis, double meanAnomalyAtEpoch, double epoch)
{
var celestialBody = FlightGlobals.Bodies.First(b => b.bodyName == body);
OrbitTools.OrbitDriver.orbit.Set(OrbitTools.CreateOrbit(celestialBody, semiMajorAxis, eccentricity, inclination, longitudeOfAscendingNode, argumentOfPeriapsis, meanAnomalyAtEpoch, epoch));
throw new YieldException(new ParameterizedContinuationVoid <int> (WaitForVesselSwitch, 0));
}
public static void SetCircularOrbit(string body, double altitude)
{
var celestialBody = FlightGlobals.Bodies.First(b => b.bodyName == body);
var semiMajorAxis = celestialBody.Radius + altitude;
OrbitTools.OrbitDriver.orbit.Set(OrbitTools.CreateOrbit(celestialBody, semiMajorAxis, 0, 0, 0, 0, 0, 0));
throw new YieldException(new ParameterizedContinuationVoid <int> (WaitForVesselSwitch, 0));
}
