On March 23, 1965, at 15:57:00 UTC, at the end of the first orbit, over Corpus Christi, Texas, a 1-minute 14 second burn of the Orbit Attitude and Maneuvering System (OAMS) engines gave a reverse delta-V of 15.5 meters per second (51 ft/s), which changed the orbit from 161.2 by 224.2 kilometers (87.0 by 121.1 nautical miles) (with a period of 88.3 minutes), to an orbit of 158 by 169 kilometers (85 by 91 nmi) (period of 87.8 minutes). This was the first orbital maneuver made by any crewed spacecraft.