ACEP Public Telemetry
Public-access telemetry presenting selected mission parameters, trajectory state, and event markers for high-level mission monitoring.
View ACEP Public Telemetry
The Alpha Centauri Exploratory Probe (ACEP) is an uncrewed interstellar spacecraft and the first operational vehicle within the 1gSpace mission architecture.
Operating under a continuous 1 g acceleration-deceleration profile, it departed on January 1, 2025 and is scheduled to arrive on July 12, 2028, where it will transition from cruise validation to orbital scientific operations.
Although distinct from the later mission vehicles in scale and configuration, ACEP applies the same broader architectural principles and serves as the program’s first in-flight validation of interstellar propulsion, autonomy, and long-duration systems behavior.
Public-access telemetry presenting selected mission parameters, trajectory state, and event markers for high-level mission monitoring.
View ACEP Public TelemetryFull-resolution operational telemetry exposing internal subsystem states, derived metrics, and control behavior across all mission phases.
View ACEP Premium AccessTechnical reference describing ACEP vehicle architecture, propulsion, power, thermal control, communications, and mission design.
View PDFFollowing orbital arrival, ACEP is tasked with characterizing the local operational environment, including orbital conditions, surface context, and atmospheric properties relevant to subsequent crewed and logistical mission stages.
The primary science phase is concentrated in the initial months after arrival, during which the vehicle performs sustained remote sensing, environmental assessment, and mission-context observation while operating fully autonomously under deep-space communication delays.
In addition to orbital measurements, the dedicated ACEP Atmos descent element performs a controlled atmospheric entry sequence, transmitting in-situ pressure, temperature, and composition data, together with descent-phase observational data, prior to terminal loss.
After completion of the primary science window, ACEP is capable of extended low-power orbital persistence, preserving a long-duration observation and telemetry asset while continuing to support architectural, environmental, and operational baseline definition.
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Speed 0 equals LEO velocity at 200 km altitude