Hi, so I got stuck on this problem and I really don't know what it is that I'm not doing right, so if you can please help me. Thank you 1. The problem statement, all variables and given/known data A satellite is in a circular orbit 11000 km above the Earth’s surface; i.e., it moves on a circular path under the influence of nothing but the Earth’s gravity. A) Find the speed of the satellite. The radius of the Earth is 6.37 × 106 m, and the accel- eration of gravity at the satellite’s altitude is 1.3225 m/s2 . Answer in units of km/s. B) Find the time it takes to complete one orbit around the Earth. Answer in units of s. 2. Relevant equations V= 2 pi r / T a= v^2/r T= V/ 2 pi r 3. The attempt at a solution First I found the hypotonus between the earth and the orbit so I can find the radius of the latitude of the orbit. I got 6370 km. Then I converted the acceleration from m/s2 to Km/s2 and I got: .0013225 km/s2. Then to find the velocity I did V= ((.0013225)(6370))(1/2)= 2.902 Km/s for the time I got 7.2681x10-5s. and both answers were wrong.