Artemis II

T+00:00:00 ยท Day 1 of 10 ยท Earth Orbit
Earth Apogee Perigee Orion
Trans-Lunar Injection in โ€”
Orbital altitude
โ€”km
To Moon
โ€”km
Velocity
โ€”km/h
Switch to miles
Estimated trajectory based on published NASA mission data.
Live telemetry integration coming before trans-lunar injection.