GRUS 3A, ..., 3G

GRUS 3α [AXELSPACE]

GRUS 3 is the second generation constellation of Earth observation micro-satellites developed by Axelspace. The satellites, designated GRUS-3A through GRUS-3G, are intended to expand the company’s GRUS 1 Earth observation constellation and improve the frequency and coverage of optical imaging services provided through the AxelGlobe platform.

The GRUS-3 satellites are designed for wide-area, high-frequency Earth observation. Operating in a 585 km sun-synchronous orbit, each satellite will be capable of revisiting the same location approximately once per day at latitudes above 25 degrees north. The spacecraft provide 2.2 m ground resolution imagery with a swath width of 28.3 km and a maximum imaging distance of 1,356 km. Collectively, the seven satellites will be able to image up to 2.3 million km² per day, significantly increasing the observation capacity compared with the earlier GRUS-1 constellation.

The satellites are manufactured by Axelspace and incorporate upgraded optical sensors with an expanded spectral range. In addition to panchromatic, blue, green, red, red-edge, and near-infrared bands used on GRUS-1, the new satellites add a Coastal Blue band for shallow-water and coastal observations. This capability supports applications such as seabed mapping and monitoring of seaweed beds while maintaining support for vegetation analysis and natural-color imaging. The satellites also employ the company’s attitude control technology to support tasking operations for targeted observations.

Each GRUS-3 satellite has a mass of approximately 150 kg and dimensions of 96 cm × 78 cm × 126 cm. The spacecraft are optimized for commercial Earth observation applications including precision agriculture, forestry monitoring, mapping, environmental monitoring, and security-related imaging services. The seven satellites are .

The satellites are scheduled for launch from Vandenberg Space Force Station in California aboard a Falcon 9 operated by SpaceX as part of the Transporter-17 rideshare mission. Launch integration services are being provided by Exolaunch.

Nation: Japan
Type / Application: Technology
Operator: AXELSPACE (GRUS)
Contractors: AXELSPACE
Equipment:
Configuration:
Propulsion:
Power: Solar cells, batteries
Lifetime:
Mass: 150 kg
Orbit: 586 km × 597 km, 97.75°
Satellite COSPAR Date LS Launch Vehicle Remarks
GRUS 3A 2026-156S 05.07.2026 Va SLC-4E Falcon-9 v1.2 (Block 5) with CAS500 4, Pelican 11, EarthDaily 8, ICEYE X77, X79, X80, X81, GRUS 3A, ..., 3G, MISR-D 1, 2, Hyperion GR1, Argonaut Demo, FireSat 1, 2, 3, Pirx 1, Kita 36, 53, Anduril-216, ION-SCV 023, Lusíada 5, 6, 7, Balkan 3, GHGSat C16, C17, Centauri 9, GRITSS, LEONAV 1, SCION-X, BRO 31, CuBy 1, ..., 5, Replicator 2, Deloitte 4, 5, 6, GENIEedge P-Body, RAFS Cubesat, CloudCT Precursor, CyberCUBE, FossaSat 2E26, IPOS-TDSM, KOYO, MAVERIC, MARMOTSat, Sentinel 1, SUCHAI 4, TOM 1, 2, 3, BOHR, Kostka, Marina, ET 001A, ..., 001D, SPEAR 1A, 1B, 1C, Lemur-2 259, ..., 263, Nova 1, Oasis Alpha, Posidònia, R5 S9
GRUS 3B 2026-156BB 05.07.2026 Va SLC-4E Falcon-9 v1.2 (Block 5) with CAS500 4, Pelican 11, EarthDaily 8, ICEYE X77, X79, X80, X81, GRUS 3A, ..., 3G, MISR-D 1, 2, Hyperion GR1, Argonaut Demo, FireSat 1, 2, 3, Pirx 1, Kita 36, 53, Anduril-216, ION-SCV 023, Lusíada 5, 6, 7, Balkan 3, GHGSat C16, C17, Centauri 9, GRITSS, LEONAV 1, SCION-X, BRO 31, CuBy 1, ..., 5, Replicator 2, Deloitte 4, 5, 6, GENIEedge P-Body, RAFS Cubesat, CloudCT Precursor, CyberCUBE, FossaSat 2E26, IPOS-TDSM, KOYO, MAVERIC, MARMOTSat, Sentinel 1, SUCHAI 4, TOM 1, 2, 3, BOHR, Kostka, Marina, ET 001A, ..., 001D, SPEAR 1A, 1B, 1C, Lemur-2 259, ..., 263, Nova 1, Oasis Alpha, Posidònia, R5 S9
GRUS 3C 2026-156Y 05.07.2026 Va SLC-4E Falcon-9 v1.2 (Block 5) with CAS500 4, Pelican 11, EarthDaily 8, ICEYE X77, X79, X80, X81, GRUS 3A, ..., 3G, MISR-D 1, 2, Hyperion GR1, Argonaut Demo, FireSat 1, 2, 3, Pirx 1, Kita 36, 53, Anduril-216, ION-SCV 023, Lusíada 5, 6, 7, Balkan 3, GHGSat C16, C17, Centauri 9, GRITSS, LEONAV 1, SCION-X, BRO 31, CuBy 1, ..., 5, Replicator 2, Deloitte 4, 5, 6, GENIEedge P-Body, RAFS Cubesat, CloudCT Precursor, CyberCUBE, FossaSat 2E26, IPOS-TDSM, KOYO, MAVERIC, MARMOTSat, Sentinel 1, SUCHAI 4, TOM 1, 2, 3, BOHR, Kostka, Marina, ET 001A, ..., 001D, SPEAR 1A, 1B, 1C, Lemur-2 259, ..., 263, Nova 1, Oasis Alpha, Posidònia, R5 S9
GRUS 3D 2026-156BC 05.07.2026 Va SLC-4E Falcon-9 v1.2 (Block 5) with CAS500 4, Pelican 11, EarthDaily 8, ICEYE X77, X79, X80, X81, GRUS 3A, ..., 3G, MISR-D 1, 2, Hyperion GR1, Argonaut Demo, FireSat 1, 2, 3, Pirx 1, Kita 36, 53, Anduril-216, ION-SCV 023, Lusíada 5, 6, 7, Balkan 3, GHGSat C16, C17, Centauri 9, GRITSS, LEONAV 1, SCION-X, BRO 31, CuBy 1, ..., 5, Replicator 2, Deloitte 4, 5, 6, GENIEedge P-Body, RAFS Cubesat, CloudCT Precursor, CyberCUBE, FossaSat 2E26, IPOS-TDSM, KOYO, MAVERIC, MARMOTSat, Sentinel 1, SUCHAI 4, TOM 1, 2, 3, BOHR, Kostka, Marina, ET 001A, ..., 001D, SPEAR 1A, 1B, 1C, Lemur-2 259, ..., 263, Nova 1, Oasis Alpha, Posidònia, R5 S9
GRUS 3E 2026-156AF 05.07.2026 Va SLC-4E Falcon-9 v1.2 (Block 5) with CAS500 4, Pelican 11, EarthDaily 8, ICEYE X77, X79, X80, X81, GRUS 3A, ..., 3G, MISR-D 1, 2, Hyperion GR1, Argonaut Demo, FireSat 1, 2, 3, Pirx 1, Kita 36, 53, Anduril-216, ION-SCV 023, Lusíada 5, 6, 7, Balkan 3, GHGSat C16, C17, Centauri 9, GRITSS, LEONAV 1, SCION-X, BRO 31, CuBy 1, ..., 5, Replicator 2, Deloitte 4, 5, 6, GENIEedge P-Body, RAFS Cubesat, CloudCT Precursor, CyberCUBE, FossaSat 2E26, IPOS-TDSM, KOYO, MAVERIC, MARMOTSat, Sentinel 1, SUCHAI 4, TOM 1, 2, 3, BOHR, Kostka, Marina, ET 001A, ..., 001D, SPEAR 1A, 1B, 1C, Lemur-2 259, ..., 263, Nova 1, Oasis Alpha, Posidònia, R5 S9
GRUS 3F 2026-156AB 05.07.2026 Va SLC-4E Falcon-9 v1.2 (Block 5) with CAS500 4, Pelican 11, EarthDaily 8, ICEYE X77, X79, X80, X81, GRUS 3A, ..., 3G, MISR-D 1, 2, Hyperion GR1, Argonaut Demo, FireSat 1, 2, 3, Pirx 1, Kita 36, 53, Anduril-216, ION-SCV 023, Lusíada 5, 6, 7, Balkan 3, GHGSat C16, C17, Centauri 9, GRITSS, LEONAV 1, SCION-X, BRO 31, CuBy 1, ..., 5, Replicator 2, Deloitte 4, 5, 6, GENIEedge P-Body, RAFS Cubesat, CloudCT Precursor, CyberCUBE, FossaSat 2E26, IPOS-TDSM, KOYO, MAVERIC, MARMOTSat, Sentinel 1, SUCHAI 4, TOM 1, 2, 3, BOHR, Kostka, Marina, ET 001A, ..., 001D, SPEAR 1A, 1B, 1C, Lemur-2 259, ..., 263, Nova 1, Oasis Alpha, Posidònia, R5 S9
GRUS 3G 2026-156K 05.07.2026 Va SLC-4E Falcon-9 v1.2 (Block 5) with CAS500 4, Pelican 11, EarthDaily 8, ICEYE X77, X79, X80, X81, GRUS 3A, ..., 3G, MISR-D 1, 2, Hyperion GR1, Argonaut Demo, FireSat 1, 2, 3, Pirx 1, Kita 36, 53, Anduril-216, ION-SCV 023, Lusíada 5, 6, 7, Balkan 3, GHGSat C16, C17, Centauri 9, GRITSS, LEONAV 1, SCION-X, BRO 31, CuBy 1, ..., 5, Replicator 2, Deloitte 4, 5, 6, GENIEedge P-Body, RAFS Cubesat, CloudCT Precursor, CyberCUBE, FossaSat 2E26, IPOS-TDSM, KOYO, MAVERIC, MARMOTSat, Sentinel 1, SUCHAI 4, TOM 1, 2, 3, BOHR, Kostka, Marina, ET 001A, ..., 001D, SPEAR 1A, 1B, 1C, Lemur-2 259, ..., 263, Nova 1, Oasis Alpha, Posidònia, R5 S9

Launch Sites:

  • Va =   Vandenberg Space Force Base, California, USA   USA

References:

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