A body is orbitting around the earth at mean radius `9` times as great as the orbit of a geostationary satellite to how many days it will complete one revolution around the earth and what is its angular velocity ?

Explanation

To solve the problem, we need to determine the time period of a body orbiting the Earth at a mean radius that is 9 times the radius of a geostationary satellite, and then calculate its angular velocity.

### Step-by-Step Solution:

1. **Identify the Radius of the Geostationary Satellite:**
The radius of a geostationary satellite (r) is approximately 42,164 km from the center of the Earth. For our calculations, we will denote this radius as \( r \).

2. **Determine the Radius of the New Satellite:**
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