HARDWARE / PRODUCTUpdated 24 Jul 2026

XavSat PocketQubes (1P to 3P)

Xavier Space Solutions (XavSat)
XavSat PocketQubes (1P to 3P)

XavSat offers miniature PocketQubes (1P to 3P) as low-cost, high-reliability platforms for rapid orbital deployment, available as educational kits or ready-to-fly spacecraft.

Typed specifications5 values

Discloses 2 of 7 fields engineers filter by in this category (category median 3).

Mass
250 g
product page 250 g max
Form factor
PocketQube 1P
from product name · product page PocketQube 3P from product name
Power available to payload
1 W
product page

Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.

As published by the supplier12 lines, in the manufacturer's own wording
Pocketqube
1P Chassis (XavSat-1 Mission)
Payload (XavSat-1 Mission)
Quantum temperature & pressure payload
Average payload power (XavSat-1 Mission)
~ 1 W
Altitude control (XavSat-1 Mission)
Passive Bar Magnet
Mass (XavSat-1 Mission)
<250 g
Antenna (XavSat-1 Mission)
Deployable 437 MHz UHF dipole antenna
Payload data downlink (XavSat-1 Mission)
1.2kb/s (UHF)
OBC microcontroller
Atmega328P
Payload communication protocols
I²C, SPI & UART etc.
Power system features
Manages solar energy collection, battery charging & power distribution & payload subsystems. Integrates maximum power point tracking (MPPT) circuitry.
1p pocketqube kits form factor
5 cm³
1p pocketqube kits mass limit
250 g

About

XavSat PocketQubes are miniature satellites, ranging from 1P to 3P form factors, designed to provide a low-cost and high-reliability platform for rapid orbital deployment. They feature a modular architecture with standardized PCB stacks for power, processing, and communications, enabling rapid prototyping from design to flight-ready hardware. These PocketQubes are compatible with standard MR-FOD or AlbaPod deployers. Key components include an On-Board Computer (OBC) based on an Atmega328P microcontroller, a payload section supporting communication protocols like I²C, SPI, and UART, and a power system that manages solar energy collection, battery charging, power distribution, and payload subsystems, integrating maximum power point tracking (MPPT) circuitry. The XavSat-1 mission, Ghana’s first private PocketQube, is an example of their application, focusing on Earth temperature and pressure profiling. XavSat also offers 1P PocketQube Kits (XavSat-P-Kits) for educational or initial space projects, providing hands-on experience with core satellite subsystems (OBC, EPS, Radio) and allowing for quick testing in sub-orbital or simulated environments. For professional missions, Ready-to-Fly (RTF) PocketQubes (XavSat-series) are available as fully functional, integrated spacecraft with solar panels, high-reliability communication modules, and specialized payload integration tailored to specific sensors, cameras, or research experiments. These RTF versions are fully assembled and flight-proven.

Documentation

No public datasheet yet — request the datasheet / ICD from the supplier.

Source: xavsat.space ↗

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