Is there an easy formula for converting a desired inclination into a launch heading?
I have read http://www.orbiterwiki.org/wiki/Launch_Azimuth
but having a tough time understanding how to calculate
cos(i) = sin(β)cos(φ)
I have read http://www.orbiterwiki.org/wiki/Launch_Azimuth
but having a tough time understanding how to calculate
cos(i) = sin(β)cos(φ)