Physics, 05.10.2019 07:30, josephbig9

An earth-orbiting satellite has the following position and velocity vectors expressed in polar coordinates r 1,2426u, km v 4.78ug km/s determine the following parameters when the satelite is 2,000 km above the earth's surface and approaching the earth: a) orbital velocity b) flight-path angle, γ c) true anomaly, 0.

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An earth-orbiting satellite has the following position and velocity vectors expressed in polar coord...