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QUESTION
A geostationary orbit has an altitude of of 35,786 km at the equator. If the satellite is above the equator and the ground station is at the equator,...
A geostationary orbit has an altitude of of 35,786 km at the equator. If the satellite is above the equator and the ground station is at the equator, and the carrier frequency of 12GHz.
The path gain for a radio signal and wavelength is (given in attachment):
How would I go about to find the path gain in dB?
