HARDWARE / PRODUCTAdded 10 Jul 2026

MicroST

Solar MEMS Technologies
MicroST

High-precision star tracker for microsatellites with <6 arcsec XY accuracy, multi-camera support and LEO/MEO/GEO qualification.

Typed specifications55 values

Discloses 10 of 12 fields engineers filter by in this category (category median 8).

Accuracy, cross-boresight
6 arcsec
datasheet p.1 6 arcsec max
Mass
600 g
datasheet p.1
Accuracy, about boresight (roll)
48 arcsec
datasheet p.1 48 arcsec max
Envelope (L×W×H)
70 x 70 x 150 mm
datasheet p.1 70 x 70 x 150 mm Volume
Update rate
5 Hz
datasheet p.1 5 Hz 5 Hz, 10 Hz  |  10 Hz  |  10 Hz 5 Hz, 10 Hz
Max tracking rate
0.5 °/s
Nominal · datasheet p.1 2.5 °/s Angular rate, Without LiS  |  3.5 °/s Max  |  2.5 °/s Without LiS  |  3.5 °/s max · Angular rate, Max.  +1
Sun exclusion angle
36 °
datasheet p.1 36 ° <  |  36 ° max · < 36 deg
Lost-in-space acquisition time
2 s
<, from LiS · datasheet p.1 2 s max · < 2 s from LiS
Supply voltage
5 V
nom. · datasheet p.1 5 V
Power consumption
3.5 W
Nominal · datasheet p.2 3.5 W
Data interface
CAN
CAN bus (upon request) · datasheet p.1 RS-422 RS422  |  RS422 upon request  |  CAN upon request  |  Ethernet upon request
Operating temperature
-30 °C
Operating temperature · datasheet p.1 -30–50 °C  |  50 °C Operating temperature
Radiation tolerance (TID)
30 krad
datasheet p.1 30 krad TID hardness EEE
Design lifetime
12 years
>, LEO · datasheet p.1 12 years min · > 12 years LEO
TRL
8
CURRENT TRL of MICROST: 8; expected TRL 9 December 2026 · datasheet p.1
Export status
ITAR-free
ITAR FREE · datasheet p.1
Configuration
single unit
standalone configuration by default; star camera version with… · datasheet p.1
Limiting star magnitude
6.5 Mv
6.5 - 7 · datasheet p.1 6.5 Mv Star magnitude limit 6.5 - 7  |  7 Mv 6.5 - 7  |  7 Mv Star magnitude limit 6.5 - 7
Survival temperature
-40 °C
Qualification temperature · datasheet p.1 60 °C Qualification temperature
Random vibration
20 g RMS
datasheet p.1 20.1 g RMS
Satellite class
microsatellites
datasheet p.1 microsat 10-100 kg Star tracker for microsatellites
Shock qualification
1 500 g
SRS @ 2000 Hz · datasheet p.1
Detector
CMOS
datasheet p.1
Volume (with baffle)
0.88 U
datasheet p.2
Earth exclusion angle
25 °
max · < 25 deg · datasheet p.1

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 supplier13 lines, in the manufacturer's own wording
Type
Star tracker for microsatellites
Interface
Digital
Model
EM and FM
Sun exclusion angle
<32°
Supply voltage
5 V, <6 W
Temperature — qualification
-30°C to +70°C
Temperature — nominal
-20°C to +50°C
Temperature — survival
-45°C to +85°C
Vibration — sine
20 g @ 10–100 Hz
Vibration — random
20.1 gRMS
Vibration — shock
1500 g SRS @ 2 kHz
Pointing accuracy
XY (3σ): <6 arcsec; Z (3σ): <48 arcsec
Communication
RS422, CAN bus or Ethernet (upon request)

About

The MicroST is a high-precision attitude determination star tracker from Solar MEMS designed for microsatellite missions. It captures images of a star field using an internal CMOS sensor and identifies stars and constellations to determine satellite pointing with very high accuracy. Like all Solar MEMS star trackers, it is a plug-and-play system requiring no additional electronics. The modular architecture allows standalone and multi-camera configurations, making MicroST adaptable for a wide range of microsatellite missions in LEO, MEO and GEO. Its compact design, high refresh rate and autonomous operation enable precise Guidance, Navigation and Control (GNC) capabilities. Available as Engineering Model (EM) and Flight Model (FM), with RS422, CAN bus or Ethernet communications available on request.

Documentation

Need the full ICD, test reports or a specific revision? Ask the supplier directly.

Source: solar-mems.com ↗

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