Fictional Planet has a gravity of approximately 0.68g
Geostationary orbit of said fictional planet is approximately 32,000 km above the surface according to online calculator.
Spacecraft capable of approximately 3g of constant acceleration (for purposes of this discussion, ignore normal requirements for fuel and/or reaction mass).
I presume that the spacecraft will also need time to DECCELERATE, but I have no idea how much affect 0.68g of planetary gravity will have on this.
Given this information, approximately how long after launch would it take for the spacecraft to reach a space station in geostationary orbit?