3. A satellite is being injected into Earth orbit at radial distance ro = 7500 km, 8.784 km/s. Calculate the possible values of the initial flight-path angle oo such t have radius of periapsis r,= 7000 km. Remember that -90 deg
3. A satellite is being injected into Earth orbit at radial distance ro = 7500 km, 8.784 km/s. Calculate the possible values of the initial flight-path angle oo such t have radius of periapsis r,= 7000 km. Remember that -90 deg
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