Final answer:
The question involves using Kepler's laws and Newton's law of gravitation in physics to determine the characteristics of a satellite's orbit, such as its orbital radius, given the satellite's mass, orbital period, and the central body's radius.
Step-by-step explanation:
The question seems to revolve around determining the physical characteristics of a satellite's orbit based on given values such as mass, altitude, period, and the radius of the central body it orbits around, which falls into the realm of classical mechanics within physics. Specifically, the question touches upon applying Kepler's laws of planetary motion and the universal law of gravitation to find quantities like the satellite's orbital radius. To solve such a problem, one would typically use the formula that relates the square of the orbital period (T) to the cube of the radius of the orbit (r) in relation to the mass of the planet or central body (M), given in the question as T² ≈ r³ / GM, where G is the gravitational constant.