To calculate the drag force, it is assumed that the drag coefficient (CD) is typically around 2.2 and that the cross-sectional area (A) of Starlink satellites is approximately 15.45 m2 (Hardy 2020). We attempted
To calculate the mean value of the square of the integral in Eq. (C.6), we use Ito isometry(C.7)〈(∫0tdW(s)e−(t−s)/τ)2〉=〈∫0tdse−2(t−s)/τ〉=τ2(1−e−2t/τ) Finally, because the first term on the right-hand side of Eq. (C.6) is the variance ...