A satellite in geostationary orbit operates at a frequency of 14 GHz is placed at a distance of 38000km. its antenna gain is 17 dB. The flux density at receiving point at the earth station is 2.76 x10^-14 W/m² in the direction of the antenna bore sight. The earth station receiving antenna has a physical aperture area of 52 m² and aperture efficiency of 70%. Calculate:

Transmitter power from the satellite in dB

The effective isotropic radiated power in dB

Antenna gain of the earth station receiver

The path loss during the downlink transmission in dB