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