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Microsat-Size Dual-Sensor Imager for VIS and NIR Imagery from 350 km Altitude

  • Generic / Specific: Real case study
  • Company Name: Scanway Space
  • Email: space@scanway.pl
  • Partner Name: Creotech Instruments S.A., CBK PAN
  • Year of implementation: 2020-2024
  • Country of implementation: Poland
  • Technology: Earth Observation Services, Payload Development
  • Industry: Aerospace
Challenge:

Development of Poland’s largest Earth Observation instrument presented a significant challenge. The primary objective was to design a telescope capable of capturing high-resolution imagery from an unusually low orbit of 350 km, achieving a spatial resolution of approximately 1 meter per pixel across two spectral ranges: visible (VIS) and near-infrared (NIR).

Solution:

The SOP200 imager (Scanway Optical Payload), featuring a 200 mm aperture—referring to the diameter of the instrument’s primary mirror—has been designed with a highly specialized optical system. This system enables the optical beam to be split into two paths, directing each beam to separate sensors. The payload is specifically engineered for integration with a microsatellite platform.

Results:

The images obtained during the ground-based testing campaign meet the mission requirements, delivering a calculated resolution of 1.2 m/pixel from an orbit of 350 km. The mission was launched on August 16, 2024.

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