A satellite moving in a circular orbit at an altitude of 1000 km completes one revolution round the earth in 105 minutes. What is (z) its angular velocity and speed? Radius of the earth `=6.4 xx 10^(6)`m.

Explanation

To solve the problem, we need to find the angular velocity and speed of a satellite moving in a circular orbit at an altitude of 1000 km, completing one revolution around the Earth in 105 minutes.

### Step-by-Step Solution:

1. **Convert the altitude to meters:**
The altitude of the satellite is given as 1000 km. To convert this to meters:
\[
\text{Altitude} = 1000 \, \text{km} = 1000 \times 10^3 \, \text{m} = 10^6 \, \text{m}
...