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Apollo 11 nominal mission timeline

What Apollo 11 was scheduled to do, hour by hour, as set out in the Apollo 11 Flight Plan (Final, July 1 1969) — the GET-tagged “as-planned” spine against which the flown mission is measured. The plan is built on hour-wide sheets with parallel CMP / CDR / LMP activity columns and a lunar-revolution (REV) count; this article captures the lunar-surface day, where the plan and reality diverged most.

The master clock is ground elapsed time (GET) — hours:minutes:seconds since liftoff. Liftoff was 9:32:00 a.m. EDT on July 16, 1969 = 13:32:00 UTC (mission), which fixes a one-line conversion good for the whole flight:

UTC = July 16, 13:32:00 + GET; EDT = UTC − 4 h (carry the day as the hours roll past 24).

Worked: the landing (GET 102:45:40 = 4 d 6:45:40) → July 20, 20:17:40 UTC = 4:17 p.m. EDT; the first step (GET 109:24:48) → July 21, 02:56:48 UTC = 10:56 p.m. EDT, still July 20 in the U.S. — which is why American memory dates the step “July 20” while the universal clock reads the 21st. The clock-true, hour-by-hour companion for any anniversary is Follow Apollo 11 in real time.

The Flight Plan scheduled the surface stay as rest first, then walk:

  • A first rest period before the EVA. The sheets carry a 4-hour REST PERIOD and a 1-hour EAT PERIOD after landing, with a STAY/NO-STAY for EVA prep check at ~110:30 and PLSS/OPS donning through 111–112.
  • EVA: 112:30 → 115:18 GET (~2 h 40 min). “START EVA” (cabin depress, open forward hatch) at 112:30; CDR egress to the platform at 112:39 — release the MESA, turn the TV on, descend the ladder; EVA termination 114:43, hatch closed and cabin repressurized by END EVA 115:18.

The planned EVA task order (GET):

GETPlanned task
112:39CDR egress; release MESA; TV on; descend ladder
~112:50Environmental familiarization; contingency sample
113:00+LMP egress; TV deployment (carry to site, tripod, panorama)
113:19Solar Wind Composition foil deployed in the Sun
113:30Bulk sample collection; weigh, pack and seal the SRC
~113:38LM inspection; deploy the close-up camera (ALSCC)
114:00EASEP deployment — LR³ (laser reflector) and PSE (seismometer, 114:06)
~114:10Documented sample collection
114:30Retrieve & stow the SWC foil; core-tube sample; close & seal SRC
114:43EVA termination; ascend ladder
115:18Hatch closed, cabin repressurized — END EVA

This is the priority-ordered sequence the LSOP laid out (contingency → bulk → experiments → documented), and the EASEP, sampling, and SWC steps map onto the concepts that cover each in detail.

The crew flew the sequence nearly intact but moved the schedule: they took the EVA ~3 hours early, swapping it ahead of the planned rest period (actual egress 109:24 vs the plan’s 112:39), and absorbed per-task overruns by trimming the documented sample. The two ceremonial acts that became iconic — the plaque, flag, and the President’s call — appear nowhere in this nominal timeline. The full task-by-task comparison (Mission Report Table 11-I) is in Apollo 11 EVA planned vs. actual timeline; this concept is the plan side it measures against. The plan also bracketed the surface stay by the powered descent (landing ~102:45 GET) and lunar ascent (liftoff ~124:22 GET).

Beyond the surface day, the as-flown GET anchors of the full flight — read from the air-to-ground transcript and gathered in the real-time companion:

GETMilestone
000:00:00Liftoff — 9:32 a.m. EDT, July 16
000:11:45Earth orbit insertion
002:44:19Translunar injection (TLI) — outbound
076:21:56Lunar orbit insertion confirmed — “like — like perfect!”, 60.9 × 169.9 nm
100:18:04Eagle undocks — “The Eagle has wings”
102:45:40Touchdown at Tranquility Base
109:24:48The first step
111:39:13Hatch closed — EVA ends
124:21:54Lunar liftoffascent & rendezvous
128:03:12Docking with Columbia
134:37:53GO for transearth injection (TEI) — homeward
195:18:18Splashdown — ~8 d 3 h 18 m after liftoff; the transcript’s last word

A quiet sub-finding of the as-flown record: most midcourse corrections were never needed. MCC-1 was scrubbed (006:19:23), MCC-3 deleted (048:12:17), MCC-4 waived (069:18:26), MCC-6 unneeded; only MCC-2 (026:45:38, translunar) and MCC-5 (150:28:31, transearth) actually burned — a measure of how accurate the Saturn V injection and the SPS burns were.