//<summary>
//Takes in position and velocity realtive to the body being orbited
//</summary>
private void calculateInitialOrbitalElements(Vector2 position, Vector2 velocity)
{
gravityElements.Mu = GlobalElements.GRAV_CONST * gravityElements.MassiveBody.GetComponent <MassiveBodyElements>().mass;
gravityElements.Position = position;
gravityElements.velocity = velocity;
//Calculate Global Tranformation Vector
gravityElements.GlobalTransformationVector = OrbitalHelper.calculateGlobalTranformationVector(gravityElements.MassiveBody);
//Calculate eccentricity
gravityElements.Eccentricity = OrbitalHelper.calculateEccentricity(position, velocity, gravityElements.Mu);
//Determine orbit type
gravityElements.OrbitType = OrbitalHelper.determineOrbitType(gravityElements.Eccentricity);
//Calculate Mechanical Energy
gravityElements.MechanicalEnergy = OrbitalHelper.calculateMechanicalEnergy(gravityElements.Position, gravityElements.velocity, gravityElements.Mu, gravityElements.OrbitType);
//Calculate Semi Major Axis
gravityElements.SemiMajorAxis = OrbitalHelper.calculateSemiMajorAxis(gravityElements.MechanicalEnergy, gravityElements.Mu, gravityElements.OrbitType);
//Calculate SemiLatusRectum
gravityElements.SemiLatusRectum = OrbitalHelper.calculateSemiLatusRectum(gravityElements.SemiMajorAxis, gravityElements.Eccentricity, gravityElements.Perigee, gravityElements.OrbitType);
//Calculate Perigee
gravityElements.Perigee = OrbitalHelper.calculatePerigee(gravityElements.SemiMajorAxis, gravityElements.Eccentricity, gravityElements.OrbitType);
//Calculate Apogee
gravityElements.Apogee = OrbitalHelper.calculateApogee(gravityElements.SemiMajorAxis, gravityElements.Eccentricity, gravityElements.OrbitType);
//Calculate Center
gravityElements.Center = OrbitalHelper.calculateCenter(gravityElements.SemiMajorAxis, gravityElements.Perigee, gravityElements.OrbitType);
//Calculate GlobalRotationAngle
gravityElements.GlobalRotationAngle = OrbitalHelper.calculateGlobalRotationAngle(gravityElements.Eccentricity, gravityElements.OrbitType);
//Find orbital directions
gravityElements.Clockwise = OrbitalHelper.clockwiseOrbit(gravityElements.Position, gravityElements.velocity);
gravityElements.TowardsPerigee = OrbitalHelper.towardsPerigeeOrbit(gravityElements.velocity, gravityElements.Eccentricity, gravityElements.OrbitType);
//Calculate trueAnomaly
gravityElements.TrueAnomaly = OrbitalHelper.calculateTrueAnomaly(gravityElements.Eccentricity, gravityElements.Position, gravityElements.TowardsPerigee, gravityElements.Clockwise, gravityElements.OrbitType);
//Calculate Eccentric Anomaly
gravityElements.EccentricAnomaly = OrbitalHelper.calculateEccentricAnomaly(gravityElements.Eccentricity, gravityElements.TrueAnomaly, gravityElements.TowardsPerigee, gravityElements.OrbitType);
//Calculate Anomaly at current epoch
gravityElements.AnomalyAtEpoch = OrbitalHelper.calculateAnomalyAtCurrentEpoch(gravityElements.Eccentricity, gravityElements.EccentricAnomaly, gravityElements.Clockwise, gravityElements.OrbitType);
gravityElements.MeanAnomaly = gravityElements.AnomalyAtEpoch;
//Calculate Angular Momentum
gravityElements.AngularMomentum = OrbitalHelper.calculateAngularMomentum(gravityElements.Eccentricity, gravityElements.Perigee, gravityElements.SemiMajorAxis, gravityElements.SemiLatusRectum,
gravityElements.Mu, gravityElements.OrbitType);
//Calculate time at epoch
gravityElements.TimeAtEpoch = OrbitalHelper.calculateTimeAtEpoch(gravityElements.Eccentricity, gravityElements.EccentricAnomaly, gravityElements.SemiMajorAxis, gravityElements.Mu,
gravityElements.Clockwise, gravityElements.TowardsPerigee, gravityElements.OrbitType);
}