Altitude / Radius 220.4 km r = 6,598 km
Orbital Velocity 7.78 km/s Mach 25.1
Apoapsis / Periapsis 225 / 185 Eccentricity: 0.003
Remaining Propellant 84.2 % Δv Cap: 1,840 m/s
LAP 1 OF 6 ACTIVE | LOS: Starbase Relay
Inclination: 28.5° North Orbital Period: 88.6 min
Atmospheric Drag: 0.0002 m/s² Thermal Shield Status: Nominal Cold Space
Flight Objective: Execute 6 consecutive non-decayed terrestrial orbits, perform vacuum relight, and demonstrate header-tank cryo transfer required for Artemis III Human Landing System (HLS) propellant depot qualification.
Cumulative Δv Expended: 0 m/s

Why Six Orbital Laps Matter for Artemis

Unlike suborbital and transatmospheric trajectory tests (Flights 1 through 5), an operational 6-lap orbital qualification proves that the thermal protection tiles survive prolonged space exposure, reaction control thrusters maintain precise attitude over hours of coasting, and cryogenic liquid oxygen and methane remain pressurized inside internal header tanks without premature boiloff.

In-Orbit Vacuum Relight & Controlled Deorbit

To clear NASA's stringent safety criteria for human lunar missions, Starship must prove its Raptor vacuum engines can reignite reliably in microgravity after extended orbital drift. This burn provides the decisive deceleration vector necessary to drop the perigee into Earth's upper atmosphere over the targeted Indian Ocean entry corridor.

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