A satellite which is revolving around earth has minimum distance from earth equal to `r_(1)` and maximum distance equal to `r_(2)` then time period of the satellite will be ?

Explanation

To solve the problem of finding the time period of a satellite revolving around the Earth with minimum distance \( r_1 \) and maximum distance \( r_2 \), we can follow these steps:

### Step 1: Determine the Average Distance
The average distance \( r \) of the satellite from the center of the Earth can be calculated as:
\[ r = \frac{r_1 + r_2}{2} \]

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