It wasn't until I shared this frustration with a smart friend, and he pointed out that it actually is possible if the space station has a rotational period equal to its orbital period, that I realized I was wrong. The author was indeed being smarter about the science of it than I was, and had done the research. And, forget just the future part of it; the ISS actually currently flies with a specific constant relative orientation through the atmosphere so as to minimize air resistance, using, you guessed it, a rotational period equal to its orbital period, plus occasional corrective actions from gyros and thrusters.
And plus solar panels, which get realigned to minimize atmospheric drag when the Sun is behind the Earth.
This is especially true if an orbiting object has attached to a tether. Gravity gradient stabilization can keep a tether aligned to the local vertical.