Orbital period:T
Vs
speed = ||Vs|| = 2πr/T
Acceleration = ||as|| = (2π)^2 r/t^2
Geostationary Orbit
T = 24h
Acceleration => (2π)^2 r/T^2 = 3√GmeT^2/(2π)^2 = 42,000 km
GTE
Error/h1 = E/(h2-h1) = Error = E h1/(h2-h1)
“Order” of a Solves
GTE = C*h order
x = sin(t)
Ch^2new = tolerance
