Calculate the orbital inclination required to place an earth-orbiting satellite in a 1000.0 km x 1500.0 km altitude, sun-synchronous orbit.
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Calculate the orbital inclination required to place an earth-orbiting satellite in a 1000.0 km x 1500.0 km altitude, sun-synchronous orbit.
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Calculate the orbital inclination required to place an earth-orbiting satellite in a 1000.0 km x 1500.0 km altitude, sun-synchronous orbit. (answer 100.64 degrees)
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