The F9R first stage was travelling at 1.62km/s at MECO (main engine cut off), about 80km up, 90km downrange. It continued on up to 170km as it performed the boost back burn to start deceleration and return to launch site.
For comparison (such as it is) Blue Origin's New Shepherd returns from a peak of 1.28km/s and an altitude of 100km.
I suspect the first stage MECO velocities of the proposed Arianespace and ULA reusable launchers will be higher than the above. It would be interesting to see what the values/profile would be for the F9R for the launch of a geo comsat.