PixelSat I

A CubeSat built by high schoolers

Project Pixel Orbital is a fully student-led team at Stanford Online High School building PixelSat I, a 3U CubeSat targeting launch into sun-synchronous low Earth orbit in early 2027, from scratch, on an extremely limited budget.

Form factor

3U CubeSat (100×100×300 mm)

ADCS

IMU, magnetometer, and sun sensor readings are merged and fused using an Extended Kalman Filter to estimate the spacecraft's attitude (orientation). Hand-wound magnetorquers are driven through a PID controller to set the satellite's angular velocity and orientation.

Power

Our battery pack is a 7.4V lithium-ion battery pack powered by high-efficiency solar panels. The satellite runs on a 3.3V bus regulated by a custom power controller, with other (higher voltage) dedicated buses for the communications system and the magnetorquers.

Flight computer

A STM32-series processor running the RTIC framework handles all onboard operations on a single core. All code is no_std Rust. We have a Raspberry Pi Zero coprocessor for camera operations, science experiments, and doom.

Communications

Our dual-band communications system uses LoRa UHF at 435 MHz alongside S-band at 2.4 GHz. The UHF transceiver is an E-Byte LoRa module built around a Semtech SX1262 chip and connected to a tape-measure antenna that deploys in orbit via a burn wire, and we are using novel patch antenna technologies for the S-band antenna.