Hyperion GR1, ..., 7

Hyperion GR1 [Open Cosmos]

Hyperion GR-1 is the first satellite in the seven-spacecraft Hyperion GR Earth observation constellation, developed by Open Cosmos Aegean for the Greek National Microsatellite Programme. Built in Athens on a 100 kg-class platform, the satellite marks the beginning of Greece's domestic satellite manufacturing capability. It provides sub-meter panchromatic imagery, onboard artificial intelligence processing, and inter-satellite communications, while also serving as one of the first spacecraft in the OpenConstellation 1.0 network.

Hyperion GR-1 is equipped with a panchromatic imaging payload providing 90 cm ground resolution and a visible/near-infrared (VNIR) multispectral camera with 4 m resolution across blue, green, red, and near-infrared bands. The instrument has a swath width of 12.3 km and supports applications including disaster response, flood monitoring, agriculture, environmental protection, infrastructure monitoring, maritime surveillance, and security. Onboard AI performs image analysis, spectral feature extraction, and target detection to reduce data volumes before transmission to Earth.

The complete Hyperion GR constellation will consist of seven satellites carrying complementary Earth observation payloads. In addition to panchromatic and VNIR imaging, later spacecraft will introduce short-wave infrared (SWIR), hyperspectral, Automatic Identification System (AIS), and Internet of Things (IoT) payloads. The hyperspectral instruments will support applications such as crop and forest monitoring, mineral exploration, water quality assessment, and environmental compliance, while the AIS and IoT payloads will expand maritime monitoring and connected sensor services. Inter-satellite links within the constellation are designed to reduce data delivery times, enabling actionable information to be provided within approximately 30 minutes during emergency situations.

Nation: Greece
Type / Application: Earth observation
Operator:
Contractors: Open Cosmos Aegean
Equipment:
Configuration:
Propulsion: None
Power: Solar cells, batteries
Lifetime:
Mass: 72 kg
Orbit: 589 km Ũ 598 km, 97.76°
Satellite COSPAR Date LS Launch Vehicle Remarks
Hyperion GR1 2026-156Q 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, Posidōnia, R5 S9
Hyperion GR2 - 202x with ?
Hyperion GR3 - 202x with ?
Hyperion GR4 - 202x with ?
Hyperion GR5 - 202x with ?
Hyperion GR6 - 202x with ?
Hyperion GR7 - 202x with ?

Launch Sites:

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

References:

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