Artemis II marks the re-establishment of US crewed deep-space capability after a 50-year absence. As the first crewed test of the Orion spacecraft and Space Launch System beyond low-Earth orbit, the mission validates the human-rated deep-space architecture required for sustained lunar operations.
The mission signals sustained US intent to establish a permanent cislunar presence via the Gateway station programme. Four-nation crew composition (US, Canada) reflects the international partnership model underpinning the Artemis Accords framework, with implications for allied space coordination and cislunar domain awareness.
MISSION TIMELINE (PLANNED)
T+0 Β· LAUNCH
SLS Block 1 Launch
Kennedy Space Center LC-39B Β· Orion separates from ICPS upper stage Β· Trans-lunar injection burn
DAY 1β3 Β· OUTBOUND
Outbound Trajectory
Orion transits to the Moon Β· Crew life support, navigation & systems checkout Β· First crewed deep-space transit since 1972
DAY 4β6 Β· LUNAR FLYBY
Closest Lunar Approach
~9,259 km closest approach Β· Far-side communications blackout expected Β· Gravity-assist return trajectory established
DAY 6β10 Β· RETURN
Earth Return & Splashdown
Return transit Β· Orion heat shield validates re-entry at ~11 km/s Β· Pacific Ocean splashdown Β· USS San Diego recovery ship
TRAJECTORY OVERVIEW (SCHEMATIC Β· NOT SIMULATED)
LIVE COVERAGE
NASA Artemis II mission coverage and NASA TV streams are available via the feed player above.
Switch to the ARTEMIS II feed tab for dedicated mission coverage.
DEEP-SPACE MISSION LAYER Β· 1 MISSION IN REGISTRY
β All mission data sourced from NASA public information Β· Timeline is planned and subject to change Β· No telemetry is simulated Β· OSINT only
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STRATWATCH
SPACE INTELLIGENCE MONITOR
OSINT Β· NSW AU
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1. NATURE OF INFORMATION
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