sat = satellite(sc,"gpsAlmanac.txt"); The default orbit propagator when creating satellites using SEM almanac is gps. This can be verified by observing the OrbitPropagator property. Additionally, the output of the orbitalElements function contains GPS satellite-specific information. orbitProp = s...
Here, m = 200 kg , M = 10^(25) kg, R = 6.4 xx 10^(6) m h = 100 km = 0.1 xx 10^(6) m Orbital velocity of satellite is upsilon(0) = sqrt((GM)/(R + h)) (i) KE of satellite, K = (1)/(2) m upsilon(0)^(2) = (1)/(2) m (GM)/(R + h) = (1)/(2...
Homework Statement The mass of the Earth is 5.972 x 10^24 kg and its orbital radius is an average of 1.496 x 10^11 m. Calculate its linear momentum...