Official name KAZSTSAT
Alternative name KazSTSat
Cospar ID 2018-099AB
Norad ID 43783
Launch date 2018-12-03
Launch site AFWTR
Launch vehicle Falcon-9 v1.2 (Block 5)
Country/Organization Kazakhstan
Type application Earth observation
Operator Ghalam LLP
RCS size MEDIUM
Decay date ON ORBIT
Period (min) 96.24
Inclination (deg) 97.53
Perigee (km) 572
Apogee (km) 585
Eccentricity 0.0112359550561798
Mean motion (revs. per day) 14.9625935162095
Semi-Major axis (km) 6956.635
Raan (deg) 177.4232
Arg of perigee (deg) 124.4132
Shape Box
Mass (kg) 110
Height (m) 0.5
Width (m) 0.5
Depth (m) 0.5
Span (m^2) 0.5
Contractors SSTL
Equipment 22 m imager
Configuration SSTL-42 (SSTL X50)
Power Solar cells, batteries

KazSTSAT is a small satellite mission built by Surrey Satellite Technology Ltd (SSTL) for Ghalam LLP (Kazakhstan) under a contract signed in 2013.

It will be based on the new SSTL-X50 Earthmapper variant and will carry an SSTL SLIM-6 imager, providing 22 m resolution multispectral imagery with a swath width of more than 600 km for global wide-area imaging. The new SSTL-X50 Earthmapper variant combines a large volume of data storage, enhanced power generation capacity and high downlink availability to continuously image the sunlit land mass making it particularly suited to applications requiring a high temporal revisit rate, such as agricultural and flood monitoring, water quality assessment, forest monitoring and disaster management.

Under a joint development programme 14 Kazakh engineers will work alongside SSTL engineers to design and build the KazSTSAT spacecraft. In addition to the SLIM-6 imager, KazSTSAT will fly a number of Ghalam LLP developed payloads, and will join the Disaster Monitoring Constellation, which provides daily images for applications including global disaster monitoring. Environmental testing will take place at a new Ghalam LLP test facility being established in Astana, Kazakhstan.

SSTL has developed the new X50 satellite platform to provide a smaller, lighter, flexible spacecraft with enhanced systems capabilities and quality. With a mass of 50 kg, the compact, highly integrated design baselines flight-proven heritage with next-generation avionics to incorporate fully dual redundant subsystems and scaled core platform services such as power, structure, data processing, communications and high-precision attitude control.

A launch in early 2017 on a Dnepr was planned, but as Dnepr is no longer available, a new launch provider is needed. The satellite was launched on Spaceflight Industry's SSO-A multi-satellite launch on a Falcon-9 v1.2 (Block 5) rocket.

Satellite COSPAR Date LS Launch Vehicle Remarks
KAZSTSAT 2018-099AB 2018-12-03 AFWTR Falcon-9 v1.2 (Block 5) with SkySat 14, 15, Eu:CROPIS, STPSat 5, FalconSat 6, NEXTSat 1, eXCITe, SeeMe, ICEYE X2, BlackSky 2, ESEO, Hawk A, B, C, Capella 1, AISTECHSAT 2, CSIM-FD, Hiber 2, ITASAT 1, Landmapper-BC 4, ORS 7A, 7B, Al-Farabi 2, Astrocast 0.1, Audacy 0, BRIO, Centauri 1, Eaglet 1, Enoch, Flock-3s 1, 2, 3, K2SAT, KazSciSat 1, MinXSS 2, Orbital Reflector, RAAF M1, SeaHawk 1, SNUSAT 2, THEA, VESTA, PW-Sat 2, SNUGLITE, VisionCube, RANGE A, B, Elysium-Star 2, ExseedSat 1, Fox 1C, Irvine 02, JY1-Sat, KNACKSAT, MOVE 2, SpaceBEE 5, 6, 7, Suomi-100, WeissSat 1, Sirion Pathfinder 2, OrbWeaver 1, 2, SPAWAR-CAL O, OR, R