Centralized data repository of standard formatted telemetry payloads
Completed cabin oxygen purge.
Initial INS calibration at launch pad.
Verifying nominal pressure in Launch and Entry Suits.
Testing umbilicals and ground station telemetry loops.
Loaded translunar target parameters into flight computer.
Voice checks with Launch Control Center completed.
Checking center of gravity and stowage for science payloads.
Crew has successfully ingressed the Orion capsule.
Final pre-launch baseline medical telemetry recorded.
Brief anomaly in temperature sensor on umbilical, self-resolved.
Cabin pressure shifting to orbital settings as external pressure drops.
Solid Rocket Boosters separated 0.2 seconds later than optimal. No structural impact.
Passed through maximum dynamic pressure with solid telemetry.
Logging launch vibration data for structural analysis.
All crew members reporting nominal under launch G-forces.
Cabin acoustic and G-load profiles within expected limits.
Pitch and roll program executed perfectly clearing the tower.
Launch Abort System and forward fairings cleanly separated.
Handing over communications from Florida to Bermuda tracking stations.
MECO achieved precisely on timeline.
Thermal loop B showed minor pressure fluctuation, stabilizing.
Orion is in a stable 100x100 nm Earth parking orbit.
Locked onto Tracking and Data Relay Satellite System.
First live video downlink from orbit established.
First on-orbit meal preparation underway.
Crew is adapting to microgravity, removing launch suits.
Solar arrays fully deployed and generating nominal power for ECLSS.
Uncapped optical navigation sensors for star tracking.
Executed small burn to circularize orbit before TLI.
Primary scrubbers online and maintaining cabin PCO2.
Switched to Deep Space Network for high-gain communications.
Star tracker temporarily blinded by debris, switched to secondary.
Passing through Van Allen belts, monitoring radiation spikes.
Captured 'Blue Marble' images for atmospheric science reference.
Completed PAO educational streaming event from half-way to the moon.
Calculated minor MCC-1 burn parameters for precise lunar targeting.
First crew shift entering sleep period.
Assembled flywheel exercise device for transit health.
Sampled potable water dispenser, chemistry is nominal.
TLI burn complete. Escaping Earth gravity well.
Crew reviewing visual observation targets for the far-side pass.
Momentary 5-second telemetry drop as we cross the Earth-Moon gravity boundary.
Adjusting thermal controls due to changing solar angles near moon.
Calibrating sensors in preparation for lunar magnetic field sweep.
Optimizing HGA pointing ahead of the flyby.
Cycling waste management system prior to high-workload flyby phase.
Activated mass spectrometer to sample tenuous lunar exosphere.
Optical navigation confirmed lunar limb coordinates.
Trajectory confirmed strictly free-return, no insertion burn required.
Preparing for Loss of Signal as Orion travels behind the moon.
Adjusted radiators for deep space viewing after lunar passage.
Mapping unlit craters using infrared spectrometry.
Captured iconic Earthrise image over the lunar horizon.
Minor, expected radiation dose rate increase observed.
Passed lowest altitude point over the lunar far side.
Acquisition of Signal! We are back in contact with Earth.
Lunar gravity formally slinging spacecraft back toward Earth.
Current status: Loss of Signal. Operating autonomously.
Running on battery power during lunar eclipse period.
Crew visually confirming geological features on the lunar surface.
Checking biological samples after deep space exposure.
Establishing communication link with US Navy recovery ships.
Crew has put the Launch and Entry Suits back on.
Downlinking all high-resolution science data recorded during LOS.
Stowing loose items and preparing cabin for reentry.
Finalizing coordinates for the 400,000 ft entry interface.
Audited remaining water, O2, and LiOH filters.
Executed small burn to refine the Earth entry corridor.
Crew performing fluid loading protocol to prepare for Earth gravity.
Reaction control thruster showed transient high temp, cleared.
Dipped out of atmosphere to bleed heat, re-entering for final descent.
Opened cabin air valves at 10,000 feet to equalize pressure.
GPS and voice comms re-established with recovery forces.
Sensors recording ablation rate of the Avcoat heat shield.
Main chutes deployed. Contact with the water confirmed.
Entering expected communications blackout due to plasma sheath.
Capsule running entirely on internal survival batteries.
Umbilicals severed, Service Module cleanly separated.
Crew experiencing peak deceleration loads.
Drogue chutes reefed slightly slower than expected, but holding.