add note about eccentricity vector

src/game.cpp

@@ -258,6 +258,12 @@ applyManeuver(GameOrbit* orbit, double previous_true_anomaly)
 	dvec3 pos = orbitGetPositionVector(r, theta);
 	dvec3 vel = orbitGetVelocityVector(mu, h, sys.elements.e, theta);
 
+	// FIXME: need to count rotation from the 'I' axis on equatorial orbits
+	// WIP
+	// also need to get the updated eccentricity vector before we can calculate
+	// 	the other angular orbital elements
+	//sys.elements.omega = sys.elements.nu;
+	// WIP
 	sys.rotation = orbitGetXForm(sys.elements);
 	sys.sat.position = sys.rotation * pos;
 	sys.sat.velocity = sys.rotation * vel;

src/main.cpp

@@ -11,7 +11,7 @@
  * - Hohmman transfer orbits
  * - make an 'overlay' graphic for things like apoapsis, perisapsis, f1, f2,
  *   	flight path
- *		- fix coordinate directions overlay 
+ *		- fix coordinate directions overlay
  * - patched conic method for transferring between 2 grav bodies
  * - test parabolic/hyperbolic trajectories
  * - organize orbit functions into interface/internal functions