To calculate the height of a satellite above Earth's surface with a speed of 7600 m/s, the relationship between orbital velocity and radius is essential. The formula v = SQRT(G.M/R) can be used, where G is the gravitational constant, M is Earth's mass, and R is the distance from the satellite to Earth's center. First, compute the orbital radius using the given velocity. Once the orbital radius is determined, the altitude can be calculated by subtracting Earth's radius from this value. Understanding these relationships is crucial for accurate satellite height calculations.