Final answer:
The radius of a geosynchronous Earth satellite orbit can be calculated using a formula. The correct radius is option c) 4.23 x 10^7 m.
Step-by-step explanation:
The radius of a geosynchronous Earth satellite orbit can be calculated using the formula:
radius = cube root of (period^2 * gravitational constant * mass of Earth / 4π^2)
Using this formula, we can calculate the radius for each option and determine the correct answer.
For option a) the radius is 4.22 x 10^7 m, for option b) the radius is 5.76 x 10^7 m, for option c) the radius is 4.23 x 10^7 m, and for option d) the radius is 6.67 x 10^7 m.
Therefore, the correct answer is option c) 4.23 x 10^7 m.