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KazEOSat-2 Satellite

6.5-m, 5-band medium-resolution KazEOSat-2 satellite imagery is the answer to your regional mapping needs.

The KazEOSat-2 Advantage

Wide Scene Footprint

KazEOSat-2 has a wide view and is ready to keep an eye on your regional projects with its 77-kilometer wide footprint and 6.5-meter resolution.

5-Band Medium-Resolution Imagery

Collecting 6.5-meter multispectral (MS) imagery, KazEOSat-2 is the perfect solution for large-area change detection, monitoring and spectral analysis.

An Affordable Solution

With a 500 square kilometer (sq km) minimum order size and affordable per sq km pricing, KazEOSat-2 leads the way in medium-resolution optical satellite imagery.

Overview & History

The Kazakhstan National Space Agency launched KazEOSat-2 on June 19, 2014 from the Yasny Cosmodrome in the Dombarovsky region of Russia. KazEOSat-2 is Kazakhstan’s first commercial medium-resolution satellite and was preceded by KazEOSat-1, it’s 1-meter (m) high-resolution counterpart. This medium-resolution satellite collects 6.5-m five-band (i.e. blue, green, red, red-edge and near-infrared) multispectral imagery.

With a 77-kilometer (km) wide footprint and strips up to 1,925-km long, KazEOSat-2 amasses an impressive 1,000,000 square kilometers of imagery daily. When it comes to large-area monitoring projects, price is often a barrier, but enter KazEOSat-2, an affordable option for high-quality regional mapping data.

KazEOSat-2 Specifications

Launch Details
  • Launch Date: June, 20, 2014, 19:11:01 UTC
  • Vehicle: Dnepr-1
  • Site: Yasny Cosmodrome, Dombarovsky region, Russia
  • Expected Mission Life: at least 7 years
KazEOSat-2 Components
  • Satellite Model: SSTL-150, built by Surrey Satellite Technology (SSTL)
  • Dimensions: 700 millimeters (mm) x 800 mm x 900 mm; 185 kilograms (kg)
  • Solar Array: 1.184 square meters (sq m) of InGaP/GaAs/Ge, 0.438 sq m of GaAs/Ge solar panels; 17.4 Ahr battery
  • Control Systems:
    • 3-axis stabilized
    • Actuators–four SSTL-100SP-M reaction wheels (one failed), three magnetorquer rods
    • Altitude determination–Rigel-L star trackers, sun sensors and SGR-7/10 GPS
  • Onboard Storage Capacity: 16 gigabytes (GB)
  • Ground Communication Systems:
    • Imagery & metadata downlink–160 Mbits per second, X-band
    • Commands & telemetry–S-Band
  • Focal Plane:
    • Multispectral CCD linear arrays with 12,000 pixels (5 arrays in parallel, 1 for each spectral band); triple line CCD’s with 3 x 12,000 pixels in a ceramics baseplate with pixel size of 6.5 micrometers (µm)
  • Optical Sensor Assembly: 633-mm focal length, 145-mm diameter aperture
Orbit Characteristics
  • Altitude: 630 kilometers (km)
  • Period: 97 minutes
  • Inclination: 98°
  • Direction: sun-synchronous circular, north to south (across the lit side of Earth)
  • Equatorial Crossing Time: 10:30 local time (approximate; across lit side of Earth)
  • Average Revisit Frequency:
    • ±30° off-nadir–4 days
    • ±17° off-nadir–8 days
Imaging System
  • Spectral Bands:
    • 5-band multispectral (blue, green, red, red-edge and near-infrared [NIR])
  • Sensor Resolution:
    • At nadir–6.5 m
    • 15° off-nadir–6.85 m
    • 30° off-nadir–8.08 m
  • Spectral Band Wavelength Range: (in nm)
    • Blue–450 to 520
    • Green–530 to 600
    • Red–620 to 690
    • Red-edge–690 to 730
    • NIR–760 to 890
  • Dynamic Range: 12-bits
Collection Capabilities
  • Footprint Width: 77 km (at nadir)
  • Maximum Collection Geometry: (at 30° off-nadir)
    • Mono, long strip–77 km x 1,925 km (1 scene wide, 1 strip long)
    • Mosaic, large area–90 km x 77 km (2 adjacent image scenes)
    • Stereo, large area–90 km x 77 km (2 fully overlapping image scenes)
  • Retargeting Ability: 37 sec (time to slew 30 degrees, fast response mode)
  • Daily Collection Capacity: 1,000,000 sq km
  • Georeferenced Horizontal Accuracy: 30-m CE90 (global average, dependent on terrain and nadir pointing)

Pricing

Data Source

archive

Minimum Order Size

500 sq km (per area & date)

Product Type

RPC controlled + 5-band MS

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