startTime = datetime(2024,4,30); stopTime = datetime(2024,5,1); sampleTime = 60; semiMajorAxis = 10000000; eccentricity = 0.1; inclination = 10; rightAscensionOfAscendingNode = 20; argumentOfPeriapsis = 30; trueAnomaly = 40; sc = satelliteScenario(startTime,stopTime,sampleTime); sat = ...