Ok, let's have another go. I take
@Sagittarius A-Star's point about the aberration.
Work in the rest frame of the planet, which I will call the primed frame for consistency with previous notation. The rocket is instantaneously moving in the -x direction and emits a very short laser pulse towards the planet. The rocket initially has four momentum ##(\gamma m,-\gamma mv,0)##, where I'm suppressing the ##z## direction. The emitted pulse has ##(E',0,-E')## and, conserving four momentum, the rocket finally has ##(\gamma m-E',-\gamma mv, E')##.
I'm going to pause here. The rocket is no longer in the same orbit, so this little instantaneous laser shot isn't correct for the original experiment. What does the rocket have to do to maintain its speed and direction? Easy solution: transform to the frame where the rocket was initially at rest. In that frame, the rocket has final four momentum ##(m-\gamma E',-\gamma vE',E')##.
I'm out of time. But the rocket is going to have to do something complicated. If it's tethered to something (e.g. an identical rocket and laser 180° away in the same orbit) the tether will no longer be straight. Or it's going to have to fire rockets to hold orbit. Either way my initial calculation was naive.