I believe they had a failure of the KU side antennas complete deployment, right after the sat was placed in orbit. So, they deployed partially, giving the odd skew.
At least I think i read that somewhere.
NewsTruck who worked in an uplink truck posted a while back about the skew:
The guy who works for SES who posts on the Fridge says that it was set at an angle as an attempt to combat rain fade. It didn't work.
I don't know if I buy that. I can't imagine why a company engaged in the aerospace industry couldn't come up with enough computer power to simulate the effect rather than just going ahead and launching a satellite based on an unproven theory!
I would like to know more about the physical/mechanical construction of a satellite, and how they are positioned and deployed.
Had always assumed that since the operators could adjust the position of the bird "in the box" that they could also "rotate" the bird (or just the transponders) to adjust the polarization, if need be.
Guess that if the sat has C & Ku band transponders, and if they actually, say, "fold them out" of the body of the sat after it is placed in orbit, and in this case (103W) the C-band portion folded out correctly and the Ku band didn't, that could have been the problem.
If I am correct in thinking that the sat operators can rotate the whole satellite (and therefore change the transponder orientation), they may have had a choice on 103W...either do what they did and leave the sat oriented with a 26 degree Ku misalignment...or rotate it to where the Ku alignment is correct and have the 26 degree issue with the C-band side.
Very interesting thread, this is something I have wondered about since I first learned of it.
