Mass:
0.8 kg
Dimensions:
96 x 90 x 119 mm^3
GSD:
14 m (@ 500km)
Swath Area:
57 x 43 km (@ 500km)
Aperture Size:
65 mm
Spectral Bands:
VIS-NIR
Instantaneous Field Of View:
5.77 degrees
Field Of View:
6.4 x 4.9 degrees
Pixel Resolution:
4096 x 3072 pixels
Pixel Pitch:
5.5 um
Focal Length:
200 mm
Focal Ratio:
3
Data Format:
8 bit
Data Format:
10 bit
Data Format:
12 bit
Data Interface:
I2C
Data Interface:
SPI
Data Interface:
LVDS
Voltage Supply:
12V
Voltage Supply:
5V
Required Power:
5 W

The SOP 1U/65 (Scanway Optical Payload) is a nanosatellite-size imager fitted to 1U designed for advanced Earth Observation applications. It is capable of capturing high-resolution imagery in both the visible (RGB) or NIR/PAN spectral bands. Operating from an altitude of 500 km, the SOP 1U/65 delivers a submeter ground sampling distance of near 14 m/pixel, ensuring detailed spatial resolution for a wide range of observational and analytical needs.

Applications

The imager facilitates a wide range of Earth observation
applications across various sectors, including:

  • Climate Change Studies
  • Urban Planning and Development
  • Agricultural Optimization
  • Forestry Management
  • Marine and Water Bodies Monitoring

Customization

Product customization is available, encompassing:

  • Number of spectral bands - by custom spectral filter application,
  • GSD / SWATH - change of camera to a different one / to our custom solution, change of optical system.

Flight heritage
The payload will be launched in the middle of the 2025.

Scanway Optical Payload 1U/65

Scanway

The SOP 1U/65 (Scanway Optical Payload) is a nanosatellite-size imager fitted to 1U designed for advanced Earth Observation applications. It is capable of capturing high-resolution imagery in both the visible (RGB) or NIR/PAN spectral bands. Operating from an altitude of 500 km, the SOP 1U/65 delivers a submeter ground sampling distance of near 14 m/pixel, ensuring detailed spatial resolution for a wide range of observational and analytical needs.

Applications

The imager facilitates a wide range of Earth observation
applications across various sectors, including:

  • Climate Change Studies
  • Urban Planning and Development
  • Agricultural Optimization
  • Forestry Management
  • Marine and Water Bodies Monitoring

Customization

Product customization is available, encompassing:

  • Number of spectral bands - by custom spectral filter application,
  • GSD / SWATH - change of camera to a different one / to our custom solution, change of optical system.

Flight heritage
The payload will be launched in the middle of the 2025.

Mass:
0.8 kg
Dimensions:
96 x 90 x 119 mm^3
GSD:
14 m (@ 500km)
Swath Area:
57 x 43 km (@ 500km)
Aperture Size:
65 mm
Spectral Bands:
VIS-NIR
Instantaneous Field Of View:
5.77 degrees
Field Of View:
6.4 x 4.9 degrees
Pixel Resolution:
4096 x 3072 pixels
Pixel Pitch:
5.5 um
Focal Length:
200 mm
Focal Ratio:
3
Data Format:
8 bit
Data Format:
10 bit
Data Format:
12 bit
Data Interface:
I2C
Data Interface:
SPI
Data Interface:
LVDS
Voltage Supply:
12V
Voltage Supply:
5V
Required Power:
5 W

The SOP 1U/65 (Scanway Optical Payload) is a nanosatellite-size imager fitted to 1U designed for advanced Earth Observation applications. It is capable of capturing high-resolution imagery in both the visible (RGB) or NIR/PAN spectral bands. Operating from an altitude of 500 km, the SOP 1U/65 delivers a submeter ground sampling distance of near 14 m/pixel, ensuring detailed spatial resolution for a wide range of observational and analytical needs.

Applications

The imager facilitates a wide range of Earth observation
applications across various sectors, including:

  • Climate Change Studies
  • Urban Planning and Development
  • Agricultural Optimization
  • Forestry Management
  • Marine and Water Bodies Monitoring

Customization

Product customization is available, encompassing:

  • Number of spectral bands - by custom spectral filter application,
  • GSD / SWATH - change of camera to a different one / to our custom solution, change of optical system.

Flight heritage
The payload will be launched in the middle of the 2025.

Current Stock:
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