HARDWARE / PRODUCTUpdated 24 Jul 2026

Infrared (IR) Earth Horizon Sensor

CubeSpace ADCS
Infrared (IR) Earth Horizon Sensor

The CubeSense Earth is a compact and reliable infrared earth horizon sensor providing high-accuracy nadir determination for satellite control, especially in eclipse, without needing a star tracker.

Typed specifications9 values

Discloses 2 of 8 fields engineers filter by in this category (category median 4).

Mass
18 g
product page
Envelope (L×W×H)
35x24x20 mm
product page
Field of view
90 °
product page 90 °
Supply voltage
3.3 V
product page
Power consumption
0.28 W
product page 0.2 W
Radiation tolerance (TID)
24 krad
product page
Connector
Molex Pico-Lock Plus
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 supplier17 lines, in the manufacturer's own wording
Accuracy (*)
1° (roll and elevation) 3-sigma
Max slew rate (°/s)
14
Mass
18 g
Dimensions [wxhxl]
35x24x20 mm
Detection field of view [°] (Horizontal/vertical)
90/80
Detection field of view [°] (Diagonal)
90
Data bus*
CAN/UART/RS-485 **I2C available for custom solutions
Connector
Molex Pico-Lock Plus
Update rate
Up to 2 Hz
Supply voltage
3.3 V
Peak power
280 mW
Average power
200 mW
Radiation
24 kRad
Random vibration
14.16 g RMS (NASA GEVS)
Thermal vacuum
-20 to 80 °C
Thermal cold and hot start
-35 to 70 °C
Design life
5+ Years

About

The CubeSense Earth is a compact and reliable infrared earth horizon sensor designed to provide high-accuracy nadir determination throughout the entire orbit. This capability is crucial for accurate satellite control during eclipse periods, offering a less expensive alternative to star trackers. Each unit undergoes rigorous verification using CubeSpace’s in-house infrared lens calibration and earth emulator jig. The sensor features an integrated processor to reduce the processing demand on the ADCS computer, a common node design, and shares electronic design and heritage across the Gen2 product range. It is qualified for space environments with specifications including 14.16 gRMS random vibration, 24 kRad radiation tolerance, and a lifetime of 5+ years. It supports various data buses like CAN, UART, and RS-485, with I2C available for custom solutions, and uses a Molex Pico-Lock Plus connector.

Documentation

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

Source: www.cubesatshop.com ↗

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