ΞĐ (Seeth) Framework Derivation of Anderson's Flyby Anomaly Constant from First Principles K = 2ωR/c General Emergence Theory Ξ = E Prime (+/−/=) · Đ = DSO (Drag-Scale-Object) ΞĐ₀ = Seeth's Constant = 6.626 × 10⁻³⁴ Anderson et al. (2008) reported anomalous velocity changes during six Earth flybys. They proposed an empirical formula with a fitted constant K = (3.099 ± 0.928) × 10⁻⁶. No physical mechanism was identified. This paper derives K from first principles within the ΞĐ (Seeth) framework: K = 2ωR/c, where ω is Earth's angular velocity and R is Earth's mean radius. The derived value K = 3.099342 × 10⁻⁶ matches Anderson's fitted value to four significant figures (ratio 1.0001). The physical mechanism is a rotating gradient density field coupling to spacecraft velocity at the relativistic rate v/c. The complete prediction includes an N-body density overlap correction that explains discrepancies in flybys where the declination-dependent primary term is small. Validation uses NASA JPL HORIZONS ephemeris data for the Galileo I flyby of December 8, 1990. Zero free parameters. Zero fitting.
Joe William Garrett (Thu,) studied this question.