Final answer:
The circumference of the satellite's orbit is found by adding Earth's radius to the satellite's distance from Earth's surface to get the total orbit radius of 10000 km and then using the formula C = 2πr. The answer is approximately 62832 km after rounding to the nearest whole kilometer.
Step-by-step explanation:
The student asked for the circumference of a satellite's orbit which is 3600 kilometers from the Earth's surface, with the Earth having a radius of approximately 6400 km. To find the circumference of the satellite's orbit, we first determine the total radius of the orbit by adding the Earth's radius to the satellite's orbital distance from the Earth's surface:
Total orbit radius = Earth's radius + Orbital distance = 6400 km + 3600 km = 10000 km.
Now, we use the formula for the circumference of a circle, which is C = 2πr, where C is the circumference and r is the radius:
Circumference of the satellite's orbit = 2 x π x 10000 km ≈ 2 x 3.14159 x 10000 km ≈ 62831.85 km.
After rounding to the nearest whole kilometer, the circumference of the satellite's orbit is approximately 62832 km.