Can anyone explain why they placed the satellite in 295x80 000 km orbit? Is it especially hard to place satellites directly into geostationary orbit, or something else?
The reason they temporarily raise their apogee so high is that it reduces the delta-v cost of changing inclination. The cost of changing inclination is directly proportional to your speed at the moment when you do the inclination change. When you are in a highly eccentric orbit, your speed at apoapsis is much lower than your speed in a circular orbit. Also, inclination burns can be combined with raising periapsis, wh…
And if you like Kerbal Space Program, but you find it isn't quite sadistic enough, go download Orbiter.