CubeSTEM MissionLab Twin

M3-B Integrated Mission Runtime · Practice only

Integrated engineering evidence

Orbit, attitude, power, communications and data

Zero measured channels

Mission time

— s

Pointing error

—°

Battery state

—%

Stored data

— Mb

Solar generation

— W

Load

— W

Link margin

— dB

Station state

Not visible

Current coupled state

Position—

Illumination—

Safe modeInactive

Wheel saturationNone

Antenna off-boresight—°

Ground elevation—°

Run metrics

Minimum battery—%

Mean pointing error—°

Generated data— Mb

Downlinked data— Mb

Overflow data— Mb

Artifact hash—

Fidelity boundary

Teaching five-face solar geometry, battery and load logic, +Z antenna boresight, free-space path loss and simplified noise margin. No CAD-confirmed panel layout, detailed EPS, modulation/coding, atmospheric RF loss, licensing, operational prediction or flight qualification claim.