A space station is in a 245-km circular earth orbit inclined at 300. The right ascension of its node line is 400. Meanwhile, a spacecraft has been launched into a 280-km by 250-km orbit inclined at 30.10, with a nodal right ascension of 400 and argument of perigee equal to 600. When the spacecraft's true anomaly is 400, the space station is 990 beyond its node line. At that instant, the spacecraft executes a delta-v burn to rendezvous with the space station in (precisely) tf hours, where tf is either selected by you or assigned by the instructor. Calculate the total delta-v required and sketch the projection of the rendezvous trajectory on the xy plane of the space station coordinates.