Space Hardware Marketplace

Sich Earth Observation Satellites

• DesignerYuzhnoye Design Office
• ManufacturerPivdenmash (Yuzhmash)
• First launch (Sich-1)31 August 1995

Series of Ukrainian Earth observation satellites designed by Yuzhnoye and manufactured by Pivdenmash (Yuzhmash), including Sich-1 and Sich-1M.

Cyclone-4M

• Height38.7 m
• Diameter4.0 m
• First stage mass260,700 kg

Two-stage light-lift launch vehicle in development by Yuzhnoye in partnership with Canada's Maritime Launch Services.

Dnepr Rocket

• Height34.3 m
• Diameter3 m
• Liftoff mass211,000 kg

Commercial satellite launch vehicle converted from the retired R-36M (SS-18 'Satan') ICBM, designed by Yuzhnoye.

Zenit Launch Vehicle

• Height57–59.6 m
• Diameter3.9 m
• Liftoff mass444,900–462,200 kg

Medium-lift orbital launch vehicle family designed by Yuzhnoye, flown as Zenit-2 from Baikonur and as the sea-launched Zenit-3SL.

Kanopus-V-IK Infrared Earth Observation Satellite

Earth observation satellite with mid-wave infrared payload for wildfire detection from 400 km SSO, with 2000 km infrared…

Gonets-M LEO Data Relay Satellite

Store-and-forward LEO communications satellite for messaging and data relay to remote regions from 1500 km near-polar orbit.

Kanopus-V Earth Observation Satellite

466 kg sun-synchronous Earth observation satellite with 2.1 m panchromatic and 3.4 m multispectral resolution, operating from 510…

VLS / VLM-1 Orbital Launch Vehicle Program

The Veículo Lançador de Satélites (VLS) is Brazil’s national orbital launch vehicle program developed by the Instituto de…

SAC-D/Aquarius

• Orbit altitude657 km SSO
• Aquarius resolution~150 km (salinity)
• Satellite mass~1,525 kg

SAC-D/Aquarius (Satélite de Aplicaciones Científicas D) was a joint Earth observation mission developed by Argentina’s CONAE and NASA.…

SAOCOM-1B

• Orbit altitude619 km SSO
• Radar bandL-band SAR (1.275 GHz)
• Resolution (stripmap)~10 m

SAOCOM-1B is the second and final satellite of Argentina’s SAOCOM (Satélite Argentino de Observación Con Microondas) constellation, developed…

SAOCOM-1A

• Orbit altitude619 km SSO
• Radar bandL-band SAR (1.275 GHz)
• Resolution (stripmap)~10 m

SAOCOM-1A (Satélite Argentino de Observación Con Microondas 1A) is the first satellite of Argentina’s SAOCOM constellation, developed by…

Soyuz-2.1v

The Soyuz-2.1v is a light-lift launch vehicle derived from the Soyuz-2 family, replacing the four liquid-fueled strap-on boosters…

Soyuz-2.1b

The Soyuz-2.1b is an upgraded medium-lift launch vehicle featuring a more powerful RD-0124 engine on the third stage,…

Soyuz-2.1a

The Soyuz-2.1a is a medium-lift launch vehicle and the modernized version of the classic Soyuz rocket, featuring digital…

Zenit-3SL

The Zenit-3SL is a three-stage liquid-fueled rocket used for the Sea Launch program, capable of delivering up to…

Sea Launch Platform

The Sea Launch platform is a mobile, ocean-going launch facility that enables Zenit-3SL rockets to be launched from…

NANOSAT-1B

• Mass19 kg
• OrbitSun-synchronous, ~660 km
• Launch date2 July 2009

19 kg Spanish nanosatellite developed by INTA for AIS ship tracking and Earth observation, launched in 2009 as…

SEOSat-Ingenio

• Mass~750 kg
• Design orbitSun-synchronous, 670 km
• Resolution2.5 m panchromatic, 10 m multispectral

750 kg Spanish Earth observation satellite developed by Airbus Spain under INTA/CDTI direction, designed for 2.5-meter panchromatic and…