Calculate the e, a (km), T (hr), ε (km2/s2), va, and vp for a satellite orbiting Earh, with a perigee radius of 7000.0 km and an apogee radius of 70000. km. Calculate the two values of the true anomaly (in degrees) at which the altitude is 35,500. km. (partial answer: Vp = 10.175 km/s)
Calculate the e, a (km), T (hr), ε (km2/s2), va, and vp for a satellite orbiting Earh, with a perigee radius of 7000.0 km and an apogee radius of 70000. km. Calculate the two values of the true anomaly (in degrees) at which the altitude is 35,500. km. (partial answer: Vp = 10.175 km/s)
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Calculate the e, a (km), T (hr), ε (km2/s2), va, and vp for a satellite orbiting Earh, with a perigee radius of 7000.0 km and an apogee radius of 70000. km. Calculate the two values of the true anomaly (in degrees) at which the altitude is 35,500. km. (partial answer: Vp = 10.175 km/s)
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