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EagleEye [Creotech]
EagleEye is a Polish earth observation satellite built by a consortium consisting of Creotech Instruments S.A. (project leader), Scanway S.A., and the Space Research Center of the Polish Academy of Sciences (CBK PAN). The satellite was built using Creotech Instruments� proprietary HyperSat platform, which is already an essential component of a number of civil and defense projects at national and European levels.
| Nation: | Poland |
|---|---|
| Type / Application: | Earth observation |
| Operator: | Creotech Instruments S.A. (project leader), Scanway S.A., Space Research Center of the Polish Academy of Sciences (CBK PAN) |
| Contractors: | Creotech Instruments S.A. (project leader), Scanway S.A., Space Research Center of the Polish Academy of Sciences (CBK PAN) |
| Equipment: | |
| Configuration: | HyperSat bus |
| Propulsion: | None |
| Power: | Solar cells, batteries |
| Lifetime: | |
| Mass: | |
| Orbit: |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| EagleEye | 2024-149AS | 16.08.2024 | Va SLC-4E | Falcon-9 v1.2 (Block 5) | with Capella 15, Tyche, AWS, QPS-SAR 8, Van Zyl 1, Tanager 1, EagleEye, Umbra-SAR 09, 10, ICEYE X33, X39, X40, X43, �uSat 48, ..., 50, GNOMES 5, Hawk 10A, 10B, 10C, LUR 1, ION-SCV 012, Sedna 1, Lemur-2 193, ..., 196, Hubble 3, ERNST, CAKRA 1, BRO 14, 15, Connecta-IoT 1, ..., 4, CUAVA 2, Hyperfield 1A, HYPSO 2, Iperdrone.0, Kanyini, Lemu Nge, Φ-sat 2, PTD 4, PTD R, Sateliot 1, 2, 3, 4, Tomorrow S1, 2, TROOP F2, Waratah Seed 1, WREN 1, Flock-4be 1, ..., 36, GNA-3, Lemur-2 191, 192, Nightjar, QUBE, SATORO T2, TORO, UM5Sat-EOSat, UM5Sat-Ribat, Deimos, Lopen, Rock, OreSat 0.5, Gaind�Sat 1A, Pico 1B-1, ..., 9 |
Launch Sites:
- Va = Vandenberg Space Force Base, California, USA
