Earth Horizon Sensor for Nadir Tracking

SKU: EARTH HORIZON SENSOR

Earth/Horizon Sensor by PYXIS SPACE

Note : Your request will be directed to PYXIS SPACE.

EARTH HORIZON SENSOR Image

The Earth Horizon Sensor from PYXIS SPACE is a compact Earth horizon sensor designed to provide reliable nadir determination and attitude estimation for small satellite missions. By simultaneously observing the Earth's horizon in infrared and visible wavelengths, it enables accurate spacecraft orientation and supports autonomous attitude control for a wide range of orbital applications. This sensor provides attitude measurement accuracy of 1° and delivers data updates at a rate of 1 Hz, enabling dependable horizon detection and spacecraft attitude estimation. 

It supports slew rates of up to 2°/s, allowing accurate operation during controlled spacecraft maneuvers. The Earth Horizon Sensor incorporates a dual-band optical system with an infrared field of view of 80° × 120° and a visible field of view of 92° × 114°, providing robust Earth detection under varying illumination conditions. It also supports a CAN 2.0B communication interface for seamless integration with spacecraft avionics and onboard control systems.

Designed for space environments, the sensor offers radiation tolerance up to 10 krad while operating from a supply voltage range of +4.5 V to +12 V. With a power consumption of only 200 mW, it provides an energy-efficient solution for power-constrained satellite platforms. Compact and lightweight, the PYXIS SPACE Earth Horizon Sensor measures 28 × 28 × 53 mm and weighs approximately 42 g, making it ideal for nadir tracking, spacecraft attitude determination, Earth observation missions and autonomous attitude control applications.

Product Specifications

Product Details

  • Part Number
    EARTH HORIZON SENSOR
  • Manufacturer
    PYXIS SPACE
  • Description
    Earth Horizon Sensor for Nadir Tracking

General Parameters

  • Space Heritage
    Yes
  • Satellite Type
    SmallSat
  • Mass
    0.042 Kg
  • Accuracy
    1 Degree
  • Field of View
    IR : 80 x 120 Degree, VIS : 92 x 114 Degree
  • Data Acquisition Rate
    1 Hz
  • Radiation Tolerance
    10 krad
  • Supply Voltage
    4.5 to 12 V
  • Power Consumption
    0.2 W
  • Slew Rate
    2 Degree/sec
  • Operating Temperature
    -20 to 50 Degree C
  • Interface
    CAN
  • Dimension
    28 x 28 x 53 mm

Technical Documents

Space Missions - A list of all Space Missions

esa

Name Date
EnVision 30 Nov, 2031
Altius 01 May, 2025
Hera 01 Oct, 2024
Arctic Weather Satellite 01 Jun, 2024
EarthCARE 29 May, 2024
Arctic Weather Satellite (AWS) 01 Mar, 2024
MTG Series 13 Dec, 2022
Eutelsat Quantum 30 Jul, 2021
Sentinel 6 21 Nov, 2020
OPS-SAT 18 Dec, 2019

isro

Name Date
INSAT-3DS 17 Feb, 2024
XPoSat 01 Jan, 2024
Aditya-L1 02 Sep, 2023
DS-SAR 30 Jul, 2023
Chandrayaan-3 14 Jul, 2023
NVS-01 29 May, 2023
TeLEOS-2 22 Apr, 2023
OneWeb India-2 26 Mar, 2023
EOS-07 10 Feb, 2023
EOS-06 26 Nov, 2022

jaxa

Name Date
VEP-4 17 Feb, 2024
TIRSAT 17 Feb, 2024
CE-SAT 1E 17 Feb, 2024
XRISM 07 Sep, 2023
SLIM 07 Sep, 2023
ALOS-3 07 Mar, 2023
ISTD-3 07 Oct, 2022
JDRS 1 29 Nov, 2020
HTV9 21 May, 2020
IGS-Optical 7 09 Feb, 2020

nasa

Name Date
NEO Surveyor 01 Jun, 2028
Libera 01 Dec, 2027
Artemis III 30 Sep, 2026
Artemis II 30 Sep, 2025
Europa Clipper 10 Oct, 2024
SpaceX CRS-29 09 Nov, 2023
Psyche 13 Oct, 2023
DSOC 13 Oct, 2023
Psyche Asteroid 05 Oct, 2023
Expedition 70 27 Sep, 2023
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