move orbitGetXForm note to header

src/orbits.cpp

@@ -86,8 +86,6 @@ orbitGetVelocityVector(double mu, double h, double e, double theta)
 	return glm::dvec3(-1 * (mu / h) * sin(theta), mu / h * (e + cos(theta)), 0);
 }
 
-// NOTE: return transform from perifocal to grav body (IJK) coordinate system
-//	in column major format
 glm::dmat3
 orbitGetXForm(OrbitalElements elements)
 {

src/orbits.h

@@ -114,6 +114,8 @@ glm::dvec3 orbitGetPositionVector(double r, double theta);
 
 glm::dvec3 orbitGetVelocityVector(double mu, double h, double e, double theta);
 
+// NOTE: return transform from perifocal to grav body (IJK) coordinate system
+//	in column major format
 glm::dmat3 orbitGetXForm(OrbitalElements elements);
 
 inline double