Hmmm, that is a relatively high delta-v to change inclination that much (~1.5-2 km/s for a ~12-15 degree difference). On the other hand, if the shared payloads are light enough (and they very well may be, particularly if the launch is undersubscribed), the upper stage could do the orbital transfer and should have plenty of delta-v to do so (particularly with a droneship landing) considering F9 regularly does recoverable flights with many tons through 2.5km/s above LEO.