Artemis II sequence of events
Artemis II: Gereral
- Time: CET
- Time conversion: EST+ 6 = CET
- Time format: DD-MM-YYYY HH:MM:SS CET
- Pre-Rollout conference: 16-01-2026 18:00:00 CET.
- Rollout start: 17-01-2026 13:00:00 CET.
- Crew interview: 17-01-2026 15:00 CET.
- Crew (4): Commander: Reid Wiseman, Pilot: Victor Glover, Mission Specialists: Jeremy Hansen and Christina Koch
- Launch pad: KSC Launch pad, LC-39B NASA Kennedy Space Center (KSC) Including weather at KSC).
- Space Weather
- Wet Dress Rehearsals (WDR)
- 01-02-2026 02:13 CET Countdown clock start (L-48 hours, 40 minutes).
- 03-02-2026 03:00 CET Simulated launch window opens
- 03-02-2026 07:00 CET Test expected to conclude
- 03-02-2026 T-5M15S: WDR 1 terminated (scrubbed) due to a liquid hydrogen leak at the interface of the tail service mast umbilical, which had experienced high concentrations of liquid hydrogen earlier in the countdown, as well. The launch control team is working to ensure the SLS (Space Launch System) rocket is in a safe configuration and begin draining its tanks.
- 03-02-2026 NASA will target March as the earliest possible launch opportunity for the flight test.
- 03-02-2026 Crew released from quarantine,
- Launch windows (2 hours)
- Friday, 06-02-2026 03:41:00 – 05:41:00 (CET). Not used.
- Saturday, 07-02-2026 04:46:00 – 06:46:00 (CET). Not used.
- Sunday, 08-02-20260 5:20:00 – 07:20:00 (CET). Not used.
- Tuesday, 10-02-2026 06:06:00 – 08:06:00 (CET). Not used.
- Wednesday, 11-02-2026 07:05:00 – 09:05:00 (CET). Not used.
- Friday, 06-03-2026 02:29:00 – 04:29:00 (CET).
- Saturday, 07-03-2026 02:57:00 – 04:57:00 (CET).
- Sunday, 08-03-2026 04:56:00 – 06:56:00 (CET).
- Monday, 09-03-2026 05:52:00 – 07:52:00 (CET).
- Wednesday, 11-03-2026 06:48:00 – 08:43:00 (CET).
- Launch Time: DD-MM-YYYY HH:MM:SS CET. Actual. Input for timers. Start Mission Time.
- Duration: 10 days (expected).
- Splashdown: 17-02-2026 UU-MM-SS CET. San Diego (expected)
- Mission Duration: DD-UU-MM-SS
1. Rollout & Pad Operations (in DD-HH-MM-SS)
OK = Successfully completed
- T-14:00:00:00 Crew enters quarantine. This period, called the health stabilization program, typically starts about 14 days before launch. Beginning quarantine now preserves flexibility as teams work toward potential opportunities in the February launch period. At this time, the agency still has not set an official launch date as testing continues for the rocket and spacecraft. Pending the outcome of the wet dress rehearsal or other operations considerations, the crew can come out of quarantine, and re-enter 14 days before any launch date. (13-01-2026) OK
- T-07-12-00-00 Rollout planning briefing OK
- T-07-06-00-00 Mission rollout authority confirmed OK
- T-07-00-00-00 Final rollout constraints review OK
- T-06-18-00-00 Mobile Launcher transport configuration verified OK
- T-06-15-00-00 Crawler-Transporter systems inspection OK
- T-06-12-00-00 Vehicle Assembly Building high bay cleared OK
- T-06-06-00-00 High bay environmental controls stabilized OK
- T-06-01-00-00 VAB doors opened for Rollout OK
- T-06-00-45-00 Crawler-Transporter positioned under Mobile Launcher OK
- T-06-00-30-00 Crawler-Transporter positioning confirmed OK
- T-06-00-25-00 Jacking and leveling system armed OK
- T-06-00-20-00 Structural load sensors powered OK
- T-06-00-15-00 Weather constraints verified OK
- T-06-00-10-00 Lightning protection systems checked OK
- T-06-00-07-00 Communications links verified OK
- T-06-00-05-00 Rollout readiness poll conducted OK
- T-06-00-02-00 Rollout authorization signed (15-01-2026) OK
- T-06-00-00-00 Rollout begins from VAB (17-01-2026) OK
- T-05-23-55-00 Initial crawler motion verified OK
- T-05-23-50-00 Vehicle clears VAB threshold OK
- T-05-23-45-00 VAB door closure initiated OK
- T-05-23-40-00 Transport speed stabilized OK
- T-05-23-35-00 Structural monitoring active OK
- T-05-22-00-00 Crawler steering alignment check OK
- T-05-20-00-00 Mid-rollout inspection completed OK
- T-05-19-00-00 Thermal gradients reviewed OK
- T-05-18-00-00 Guidance systems alignment checked OK
- T-05-17-00-00 Crawler braking test OK
- T-05-16-00-00 Pad arrival clearance issued OK
- T-05-14-00-00 Approach corridor verified OK
- T-05-12-00-00 Vehicle approaches Launch Pad LC-39B. NASA Kennedy Space Center (KSC) OK
- T-05-11-00-00 Pad hazard area cleared OK
- T-05-10-30-00 Final crawler positioning OK
- T-05-10-00-00 Pad interface safety verification OK
- T-05-09-45-00 Mobile Launcher lowering initiated OK
- T-05-09-30-00 Mobile Launcher hard-down OK
- T-05-09-15-00 Load transfer confirmed OK
- T-05-09-00-00 Vehicle leveling confirmed OK
- T-05-08-45-00 Pad structural lock pre-check OK
- T-05-08-30-00 Pad structural locks engaged OK
- T-05-08-15-00 Structural load re-balance OK
- T-05-08-00-00 Ground power connected OK
- T-05-07-45-00 Ground power quality verified OK
- T-05-07-30-00 Data umbilicals connected OK
- T-05-07-15-00 Data path validation OK
- T-05-07-00-00 Environmental control lines attached OK
- T-05-06-30-00 Environmental flow stabilized OK
- T-05-06-00-00 Pad safety perimeter verified OK
- T-05-06-00-00 Emergency Egress, swing test crew access arm OK
2. Pad Activation, Tests & Reviews (in DD-HH-MM-SS)
- T-05-00-00-00 Pad PIA / PIPA (Pad Interface and Performance Assessment (checks interfaces between SLS/Orion and the launch pad) OK
- T-05-00-00-00 Booster servicing (hydrazine) (26-01-2026) OK
- T-05-00-00-00 Integrated vehicle power-up OK
- T-04-21-00-00 Core Stage avionics pre-power checks OK
- T-04-18-00-00 Core Stage avionics activated OK
- T-04-15-00-00 Orion avionics pre-power checks OK
- T-04-12-00-00 Orion avionics activated OK
- T-04-09-00-00 Launch Abort System controller checks OK
- T-04-06-00-00 Launch Abort System power check OK
- T-04-03-00-00 Guidance system load verification OK
- T-04-00-00-00 Guidance system initialized OK
- T-03-21-00-00 Navigation sensor warm-up OK
- T-03-18-00-00 Navigation sensors calibrated OK
- T-03-15-00-00 Star tracker alignment test OK
- T-03-12-00-00 Communications systems checked OK
- T-03-09-00-00 Voice and telemetry loop tests OK
- T-03-06-00-00 Flight termination system inspection OK
- T-03-03-00-00 Range safety data verification OK
- T-03-00-00-00 RS-25 engine controllers powered OK
- T-02-21-00-00 ICPS avionics pre-checks OK
- T-02-18-00-00 ICPS avionics activated OK
- T-02-15-00-00 Propulsion data validation OK
- T-02-12-00-00 Integrated systems health check OK
- T-02-09-00-00 Redundancy failover test OK
- T-02-06-00-00 Thermal conditioning systems active OK
- T-02-03-00-00 Countdown clock verification OK
- T-02-01-00-00 Launch team called to their stations 49 hours before launch. OK
- T-02-00-00-00 Countdown simulation initiated OK
- T-01-21-00-00 Ground system redundancy verified OK
- T-01-18-00-00 Emergency response readiness review OK
- T-01-15-00-00 Weather rule compliance review OK
- T-01-12-00-00 Range safety coordination reviewed OK
- T-01-09-00-00 Launch control system validation OK
- T-01-06-00-00 Countdown rehearsal completed OK
- T-01-03-00-00 Open work closeout OK
- T-01-03-00-00 Flight Readiness Review (FRR) (00-00-2026)
- T-00-12-00-00 Start Wet Dress Rehearsal (WDR) (00-00-2026) (No crew, hold at T-00-00-00-29)
- OR
- T-00-12-00-00 Launch preparations granted (00-00-2026)
3. Last 49 hours, Launch Day Countdown & Crew (L-00H00M00S)
L-49 hours 15 minutes and counting
- L-49H15M00S: The launch team arrives on their stations and the countdown begins.
- L-48H40M00S: The countdown clock begins.
- L-47H30M00S – L-38H30M00S: Fill the water tank for the sound suppression system.
- L-48H45M00S – L-39H45M00S: Liquid Oxygen (LOX)/Liquid Hydrogen (LH2) system preparations for vehicle loading.
- L-39H30M00S – L-38H45M00S: The core stage is powered up.
- L-40H30M00S – L-39H00M00S: The interim cryogenic propulsion stage (ICPS) is powered up.
- L-38H45M00S – L-34H30M00S: Final preparations of the four RS-25 engines.
L-34 hours 30 minutes and counting
- L-33H45M00S – L-33H10M00S: The ICPS is powered down.
- L-32H30M00S – L-28H30M00S: Charge Orion flight batteries to 100%.
- L-30H30M00S – L-23H30M00S: Charge core stage flight batteries.
- L-19H15M00S – L-17H45M00S: The ICPS is powered-up for launch.
- L-19H30M00S – L-16H00M00S: Orion crew suit regulator leak checks.
L-15 hours and counting
- L-14H30M00S – L-13H00M00S: All non-essential personnel leave Launch Complex 39B.
- L-12H45M00S – L-11H15M00S: Ground Launch Sequencer (GLS) activation.
- L-13H15M00S – L-11H05M00S: Air-to-gaseous nitrogen (GN2) changeover and vehicle cavity inerting.
L-11 hours 40 minutes and counting
- L-11H35M00S – L-9H20M00S: 2-hour 15-minute built in countdown Hold begins.
- L-11H40M00S – L-10H30M00S: Launch team conducts a weather and tanking briefing.
- L-10H20M00S: Launch team decides if they are “go” or “no-go” to begin tanking the rocket.
- L-10H20M00S – L-9H00M00S: Orion cold soak.
- L-10H10M00S – L-9H50M00S: Core stage LOX transfer line chilldown.
- L-10H10M00S – L-9H25M00S: Core stage LH2 chilldown.
L-10 hours and counting
- L-9H50M00S – L-9H10M00S: Core stage LOX main propulsion system chilldown.
- L-9H25M00S – L-9H00M00S: Core stage LH2 slow fill start.
- L-9H20M00S: Resume T-Clock from T-8H10M00S.
- L-9H10M00S – L-8H55M00S: Core stage LOX slow fill.
- L-9H00M00S – L-7H40M00S: Core stage LH2 fast fill.
- L-8H55M00S – L-6H10M00S: Core stage LOX fast fill.
- L-8H45M00S – L-8H10M00S: ICPS LH2 chilldown.
- L-8H10M00S – L-7H25M00S: ICPS LH2 fast fill start.
- L-7H45M00S – L-6H00M00S: ICPS LOX main propulsion system chilldown.
- L-7H40M00S – L-7H30M00S: Core stage LH2 topping.
- L-7H30M00S: Terminal count: Core stage LH2 replenish.
- L-7H25M00S – L-7H05M00S: ICPS LH2 vent and relief test.
- L-7H05M00S – L-6H55M00S: ICPS LH2 tank topping start.
- L-6H50M00S: Terminal count: ICPS LH2 replenish.
- L-6H10M00S – L-5H40M00S: Orion communications system activated (RF to mission control)
- L-6H10M00S – L-5H40M00S: Core stage LOX topping.
L-6 hours and counting
- L-6H00M00S – L-5H15M00S: ICPS LOX fast fill.
- L-5H40M00S: Terminal count: Core stage LOX replenish.
- L-5H15M00S – L-5H00M00S: ICPS LOX vent and relief test.
- L-5H00M00S – L-4H40M00S: ICPS LOX topping.
- L-5H40M00S: Stage pad rescue.
- L-5H40M00S: Closeout crew assemble.
- L-4H40M00S: Terminal count: ICPS LOX replenish.
- L-4H40M00S: All stages replenish.
- L-4H40M00S: Start 40-minute built in Hold.
- L-4H40M00S – L-4H25M00S: Closeout crew to white room.
- L-4H30M00S – L-4H20M00S: Crew Module hatch preps and closure.
- L-4H20M00S – L-3H20M00S: Counterbalance mechanism hatch sealpress decay checks.
- L-3H20M00S – L-2H40M00S: Crew Module Hatch service panel install/closeouts.
- L-2H40M00S – L2H20M00S: Launch Abort System (LAS) Hatch closure for flight.
- L-1H10M00S: Launch Director brief – Flight vehicle/TPS Scan results with CICE.
- L-1H45M00S – L-1H40M00S: Closeout crew departs Launch Complex 39B.
L-40 minutes and holding
- L-40M00S: Built in 30-minute countdown Hold begins.
L-25 minutes and holding
- L-25M00S: Transition team to Orion to Earth communication loop following final NTD briefing.
- L-16M00S: The launch director polls the team to ensure they are “go” for launch.
T-10 minutes and counting
- T-10M00S: Ground Launch Sequencer (GLS) initiates terminal count.
- T-8M00S: Crew Access Arm retract.
- T-6M00S: GLS go for core stage tank pressurization.
- T-6M00S: Orion set to internal power.
- T-5M57S: Core stage LH2 terminate replenish.
- T-4M00S: GLS is go for core stage auxiliary power unit (APU) start.
- T-4M00S: Core Stage APU starts.
- T-4M00S: Core stage LOX terminate replenish.
- T-3M30S: ICPS LOX terminate replenish.
- T-3M10S: GLS is go for purge sequence 4.
- T-2M02S: ICPS switches to internal battery power.
- T-2M00S: Booster switches to internal batter power.
- T-1M30S: Hold for three minutes to verify core stage certification.
- T-1M30S: Core stage switches to internal power.
- T-1M20S: ICPS enters terminal countdown mode.
- T-50S: ICPS LH2 terminate replenish.
- T-33S: GLS sends “Go for automated launch sequencer” command.
- T-33S: GLS Cutoff/Recycle.
3. Launch Day Countdown & Crew (in DD-HH-MM-SS)
- T-00-00-00-29 Stop when Wet Dress Rehearsal (WDR) The first run will begin approximately 49 hours before launch when launch teams are called to their stations, to 1 minute 30 seconds before launch, followed by a planned three-minute hold and then countdown resumption to 33 seconds before launch – the point at which the rocket’s automatic launch sequencer will control the final seconds of the countdown. Teams then will recycle back to T-10 minutes and hold, then resume down to 30 seconds before launch as part of a second run.
- T-00-00-00-29 Drain tanks (WDR)
- OR
- T-00-00-02-00 Launch Readiness Review (LRR) (00-00-2026)
- T-00-00-02-00 Polling: Go / No-Go for Launch (00-00-2026)
4. Launch & Ascent (MET in DD-HH-MM-SS)
- 00-00-00-00 Launch commit executed
- 00-00-00-03 Vehicle internal power transition
- 00-00-00-06 Hydrogen burn-off igniters activated
- 00-00-00-07 RS-25 engine ignition sequence
- 00-00-00-08 Engine health verification
- 00-00-00-10 Liftoff (launch) (Step 1)
- 00-00-00-15 Hold-down post release
- 00-00-00-20 Vehicle clears launch tower
- 00-00-00-25 Guidance closed-loop control
- 00-00-00-30 Roll maneuver initiated
- 00-00-00-40 Roll maneuver complete
- 00-00-00-45 Pitch program initiated
- 00-00-01-10 Throttle bucket entry
- 00-00-01-20 Maximum dynamic pressure
- 00-00-01-40 Throttle recovery
- 00-00-02-00 Booster tailoff
- 00-00-02-10 Solid Rocket Booster separation (Step 2)
- 00-00-02-20 Booster clearance confirmed
- 00-00-03-30 Core Stage guidance update
- 00-00-06-00 Mixture ratio adjustment
- 00-00-08-00 Core Stage propellant depletion prediction
- 00-00-08-20 Core stage Main Engine Cutoff (MECO) (Step 3)
- 00-00-08-25 Thrust termination confirmed
- 00-00-08-30 Core Stage separation
- 00-00-08-50 Separation dynamics damped
- 00-00-09-00 ICPS ignition
- 00-00-12-00 Parking orbit insertion burn complete
- 00-00-18-00 Stable parking orbit achieved
5. Earth Orbit, TLI & Lunar Flyby (MET in DD-HH-MM-SS)
- 00-00-30-00 Orbit phasing setup
- 00-01-00-00 Systems stabilization in orbit
- 00-01-30-00 Post-insertion systems checkout
- 00-01-50-00 Trans Lunar Injection (TLI) readiness review
- 00-00-00-00 Perigee raise maneuver (Step 4)
- 00-00-00-00 Apogee raise burn to high Earth orbit (Step 5)
- 00-02-30-00 Orion separation from ICPS followed by Proximity Operations Demonstration (plus manual handling qualities assessment for up to 2 hours, testing) (Step 6)
- 00-00-00-00 Perigee raise burn
- 00-00-00-00 Orion Upper Stage Separation (USS) separation (USS) burn (Step 7)
00-00-00-00 Perigee raise burn (Step 8) - 00-02-00-00 Trans Lunar Injection (TLI) burn initiated
- 00-02-10-00 Mid-burn guidance update
- 00-02-20-00 Trans Lunar Injection (TLI) burn completed (Step 9)
- 00-02-25-00 Trajectory verification
- 00-00-00-00 Apogee raise burn to high Earth orbit (begin 23,5 hour checkout of spacecraft)
- 00-02-30-00 ICPS shutdown
- 00-00-00-00 Perigee raise burn
- 00-02-45-00 Orion attitude acquisition
- 00-03-00-00 Orion autonomous flight established
- 00-00-00-00 Outbound transit to Moon. Outbound Trajectory Correction (OTC) for Lunar free return trajectory. Travel time 4 days (Step 10)
- 01-00-00-00 Translunar coast operations
- 02-00-00-00 Mid-course correction executed
- 03-00-00-00 Navigation solution update
- 04-00-00-00 Lunar approach targeting
- 04-01-00-00 Lunar far-side tracking
- 04-02-00-00 Lunar Flyby. Closest approach to Moon (10.427 km) (Step 11)
- 04-03-00-00 Free-return energy confirmation
- 04-04-00-00 Lunar gravity assist complete
- 04-06-00-00 Free-return trajectory confirmed
- 00-00-00-00 Trans-Earth Return. Return Trajectory Correction (RTC) burns as necessary to aim to Earth’s atmosphere (Step 12)
6. Earth Return, Entry & Splashdown (MET in DD-HH-MM-SS)
- 05-00-00-00 Earth return coast begins
- 07-00-00-00 Entry targeting refinement
- 08-00-00-00 Entry corridor verification
- 09-12-00-00 Crew cabin configured for entry
- 09-18-00-00 Service Module (SM) separation prep (Step 13)
- 09-22-00-00 Service Module separation executed
- 09-23-00-00 Attitude reorientation for entry
- 10-00-00-00 Entry interface (Step 14)
- 10-00-00-40 Plasma onset
- 10-00-01-00 Communications blackout begins
- 10-00-02-00 Peak deceleration
- 10-00-03-00 Peak aerodynamic heating
- 10-00-05-00 Lift modulation guidance
- 10-00-06-00 Communications blackout ends
- 10-00-07-30 Drogue deployment command
- 10-00-08-00 Drogue parachutes deployed
- 10-00-09-30 Vehicle stabilized
- 10-00-10-00 Main parachute deployment
- 10-00-11-00 Main parachutes inflated
- 10-00-13-00 Descent rate stabilized
- 10-00-15-00 Splashdown (San Diego) (Step 15)
Personnel
Artemis II Crew
- Reid Wiseman – Commander (NASA) – born 1975.
- Victor Glover – Pilot (NASA) – born 1976.
- Christina Koch – Mission Specialist (NASA) – born 1979.
- Jeremy Hansen – Mission Specialist (Canadian Space Agency) – born 1976.
Artemis II Ground Team
- John Honeycutt – Artemis II mission management team chair
- Charlie Blackwell-Thompson – Artemis launch director, Exploration Ground Systems
- Jeff Radigan – Artemis II lead flight director, Flight Operations Directorate
- Lili Villarreal – landing and recovery director, Exploration Ground Systems
- Jacob Bleacher – chief exploration scientist, Exploration Systems Development Mission Directorate
Footnote
- Sources: Aerospace dashboard, funkystuff.org
- Outgoing: NASA
- Keywords: Table, Artemis2, Artemis 2
