This is just a test Input the semi-major axis: 
Input the eccentricity of the orbit: 
Input the orbital inclination: 
Input the amount you wish to rotate: 
Calculate: 

The apogee point is (along the x-axis is:) 
The perigee point is (along the x-axis is:) 
The semi-minor axis is (along the z-axis is:) 


The x position before inclination is: 
The z position before inclination is: 


The x position after rotation about z-axis: 
The z position after rotation about the z-axis: 
The y position after rotation about the z-axis is: