1. The problem statement, all variables and given/known data Find the speed of a satellite in geosynchronous orbit? in finding the speed for geosnychronous orbit the Time is 1 day, or 24hours , 86400 seconds. I tried using T^2=4(pi)^2(r)^3/GM is the eqn. I manipluated it into: r=(GM_earth_T/4(pi)^2)1/3 Once I found r I used it as Distance and then used: V=D/T ... i think my units are wrong. When using the eqn. does ur distance come out in meters or Kilometers?