An artificial satellite takes 90 minutes to complete its revolution around the earth. Angular speed of the satellite will be what?
Given,
The time period of the satellite is,
T =90 min = (90 × 60) sec = 5400 sec
We know,
Angular speed, ω = 2πT
Putting all the values
Angular speed = 2π5400=π2700 rad/s
Hence the angular speed of the satellite is π2700 rad/sec