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An earth-orbiting satellite is in an elliptical orbit with semimajor axis 9802 km and eccentricity 0.20.If the satellite is 15 degrees past periapsis, then what
An earth-orbiting satellite is in an elliptical orbit with semimajor axis 9802 km and eccentricity 0.20.If the satellite is 15 degrees past periapsis, then what is the time since periapsis, t-T?Give your answer in minutes, with two digits to the right of the decimal place.
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