The radius and time period of orbit of a sattellite are related by the formula:

R³ = GMT²/4π²; where R is the orbital radius, T is the orbital time period, M is the mass of the more massive body, G is the graviational constant

(9.4 x 10⁶)³ = (6.674 × 10⁻¹¹<span>)(M)(2.8 x 10</span>⁴<span>)</span>²<span> / (4</span>π²)

M = 6.27 x 10²³ kg

**Answer:**

I believe the camels hooves or whatever are built diffrenet.

**Explanation:**