4.
The orbital period of a satellite in a circular orbit of 500 km above the Earth's surface, taking mean radius of the Earth as 6400 km and Kepler's constant µ as 4 × 105 km3/s2 nearly

6.
The output stage of a transponder on board a satellite has a maximum power output of 10 watts. However, it is not operated at the maximum power output in order to

7.
The maximum unambiguous range of pulsed radar depends upon

8.
Linear velocity of a satellite in a circular orbit is

9.
The mean sun does at a uniform speed but otherwise requires the same time as the real sun to complete one orbit of the earth, this time being

10.
In a pulsed radar, the peak radar transmitter power is increased by a factor of 81 keeping all other radar parameters unchanged. The maximum range capability of the radar increases by a factor of

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