Only if you deploy the sats in the prograde direction. Based on the released Vine video, at least the 2nd sat appears to have been deployed sideways-ish. Also, stage propellant blowdown during passivation probably has a bigger propulsive result than separation kick.
Great slice of news here.
http://www.nasaspaceflight.com/2015/03/spaceport-america-spacex-reusability-testing/Interestingly, that most recent mission resulted in impressive performance from the launch vehicle, with source information noting the upper stage shut down on reaching the “apogee maximum limit”, still with propellant available for additional performance, had it been required. The contracted minimum apogee was actually many thousands of miles less than what was actually achieved.
Further confirmation of Falcon 9 performance:
Peter B. de Selding (@pbdes)
13/05/2015 18:11
Eutelsat: Accuracy of March SpaceX launch of our Boeing all-elec telecom sat means it'll take just 7 months, not 8, to arrive at geo orbit.
https://twitter.com/pbdes/status/598536099892432896