| T-Plus | Event |
| 00:00 | Lift-off |
| 00:10 | Pitch and roll maneuver initiated |
| 00:15 | Roll terminated |
| 01:19 | Maximum dynamic pressure (altitude
7.8 miles, 2.5 miles downrange,
velocity 1,010 miles per hour). |
| 02:15.7 | Pitch terminated |
| 02:20.7 | First stage inboard engines cutoff |
| 02:23.7 | First stage outboard engines cutoff
(altitude 35 miles; 35 miles down-
range, velocity 4,150 mph) |
| 02:24.3 | Second stage ullage rocket ignition |
| 02:24.5 | First stage separates |
| 02:26.13 | Second stage ignition |
| 02:49.55 | Camera capsule ejected from
separated S-IB |
| 02:50 | Launch escape system Jettison |
| 02:52.55 | Initiate active guidance |
| 10:01.35 | Second stage engine cutoff (altitude
135 miles, 969 miles downrange,
velocity 14,300 mph). |
| 10:11 | Separation of spacecraft from
Saturn second stage |
| 10:22 | First burn Service Propulsion System
Engine (SPS), 215 seconds |
| 11:52 | Second stage bulkhead test begins |
| 13:57 | First burn concluded |
| 41:25 | Apogee reached, 706 statute miles |
| 1:05:38 | RCS ullage burn |
| 1:06:08 | Second burn SPS, 88 seconds |
| 1:07:36 | Second SPS burn concluded |
| 1:07:45 | Third SPS burn, 3 seconds |
| 1:07:49 | Third SPS burn concluded |
| 1:07:59 | Fourth burn SPS, 3 seconds |
| 1:08:02 | Fourth SPS burn concluded |
| 1:09:58 | CM/SM separation attitude |
| 1:11:16 | CM/SM separation sequence starts
(150 seconds RCS burn SM) |
| 1:11:17 | CM/SM separation |
| 1:11:56 | CM reentry attitude |
| 1:12:38 | CM at 400,000 foot altitude |
| 1:13:36 | Blackout begins |
| 1:23:36 | Blackout ends |
| 1:26:58 | Apex cover jettisoned |
| 1:27:00 | Drogue chute deployed |
| 1:27:52 | Main chute deployed at 10,350 feet |
| 1:32:54 | Splashdown |