We can use the formula:
time = distance/speed
where distance is the distance traveled by the signal (from the satellite to Earth's surface) and speed is the speed of the signal (given as 4.00∙10^7 meters per second).
The distance traveled by the signal is the sum of the heights of the satellite and the Earth's radius (assuming the signal travels straight down to the surface):
distance = 10.88∙10^6 meters + 6.37∙10^6 meters
distance = 17.25∙10^6 meters
Now we can plug in the values:
time = distance/speed
time = (17.25∙10^6 meters) / (4.00∙10^7 meters per second)
time = 0.43125 seconds
Therefore, it will take approximately 0.43125 seconds for a radio signal to travel from a satellite orbiting at a height of 10.88∙10^6 meters to the surface of Earth.
A radio signal travels at 4.00∙10^7 meters per second. How many seconds will it take for a radio signal to travel from a satellite to the surface of Earth if the satellite is orbiting at a height of 10.88∙10^6 meters?
Show your work.
1 answer