Starlink satellites during their orbital descent from 550 km to 480 km poses an empirical challenge to classical orbital mechanics models. Orthodox explanations, which attribute these failures to micrometeorites or hardware defects induced by residual atmospheric drag, are statistically insufficient given the spatial repeatability of the anomaly. In this work, we apply the Quantum Diffusion Framework (DQ-12) to model Low Earth Orbit (LEO) not as a classical vacuum perturbed by trailing gases, but as a continuous topological fluid medium. We demonstrate that the massive transit of thousands of satellites at hypersonic speeds induces a trail of geometric turbulence, or "phase noise." The descent to 480 km introduces the satellites into a gradient of higher topological impedance. The cross-interaction of these trails in a rigid medium causes phase friction to exceed the elastic limit of the local space. The subsequent thermodynamic relaxation of the medium discharges kinetic energy directly onto the structures, causing physical rupture. The need for "phase aerodynamics" is proposed for the design of future constellations.