Subscribe with SteadyEagleEye
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, ŅuSat 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, UM5-EOSat, UM5-Ribat, Deimos, Lopen, Rock, OreSat 0.5, GaindéSat 1A, Pico 1B-1, ..., 9 |
Launch Sites:
- Va = Vandenberg Space Force Base, California, USA
