Puchacz 🦉

Our second satellite mission. Building on success, reaching for new heights.

Puchacz Mission Patch

Meet Puchacz

Objective: To demonstrate Earth observation with multispectral imaging, demonstrate optical downlink in orbit, and give students hands-on experience with a larger satellite system.

Following the successful launch of HYPE, we're proud to announce Puchacz - our second satellite mission. This 2U CubeSat represents a significant step forward in our mission to advance Polish space technologies.

Building on the experience and lessons learned from HYPE, Puchacz will carry more advanced payloads and test cutting-edge technologies that push the boundaries of what student-built satellites can achieve.

Satellite Format: 2U CubeSat (10×10×22.7 cm)
Launch Window: 2027
Development: Faculty of Space Technologies AGH

Mission Goals

Puchacz represents a new chapter in SatLab AGH's journey. With a larger form factor and advanced payloads, this mission aims to:

  • Demonstrate Earth observation with multispectral imaging
  • Demonstrate optical downlink in orbit
  • Give students hands-on experience with a larger satellite system

This mission proves that through passion, knowledge, and collaboration, we can reach for the stars and make significant contributions to space technology!

Payloads

Earth Imaging Cameras

Puchacz carries two advanced cameras for comprehensive Earth observation:

  • RGB Camera - High-resolution color imaging for detailed visual documentation of Earth's surface
  • Multispectral Camera - Captures data across multiple spectral bands, enabling detailed analysis of vegetation, water quality, land use, and environmental monitoring

These imaging systems will enable scientific research and contribute to Earth observation capabilities from space.

DZIDA

DZIDA is a compact wide-beam optical communication transmitter flying on Puchacz. The 0.25U payload demonstrates an in-house proof-of-concept laser downlink: an infrared high-peak-power pulsed diode driven by a radiation-hardened FPGA delivers efficient transmission with low average power. Wide-beam design relaxes ADCS pointing requirements and keeps satellite-side cost down, paving the way for robust, energy-efficient optical links on future small satellite missions.

Technical Specifications

Dimensions: 10×10×22.7 cm (2U CubeSat)
Mass: <4 kg
Primary Payloads: RGB Camera, Multispectral Camera, DZIDA (optical downlink)
Development Phase: In Progress
Project Status: Active Development