The formula to calculate the orbital period (p) is:
\[ p = \sqrt{\frac{4 \pi^2 r^3}{G M}} \]
Where:
An orbital period is defined as the total time it takes a satellite or orbiting object to make one complete rotation around another larger object.
Let's assume the following values:
Using the formula to calculate the orbital period:
\[ p = \sqrt{\frac{4 \pi^2 (7.5e7)^3}{6.67430e-11 \times 5.97e24}} \approx 115.347 \times 10^3 \text{ s} \]
The Orbital Period (p) is approximately 115347 seconds.