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Vehicle: Ariane 62 | Atlas V 551 | Electron | Falcon 9 Block 5 | Falcon Heavy | Firefly Alpha | Gaganyaan Abort Test Booster | Gravity-1 | GSLV Mk. II | H3 | H3-22 | H3-24 | H3-30 | KSLV-2 Nuri | Launch Vehicle Mark-3 (GSLV Mk III) | Long March 2F/G | Long March 3B/E | Long March 8A | Minotaur IV | Miura 5 | Neutron | New Glenn | Orbex Prime | Proton-M Blok DM-03 | PSLV | RFA One | Skyrora XL | Soyuz 2.1a | Soyuz 2.1b Fregat | Soyuz 2.1b Fregat-M | Soyuz-5 | Space Launch System Block 1 | Spectrum | Starship | Themis Demonstrator | Unknown Launch Vehicle | Vega-C | Vulcan | Vulcan VC6L
Orbit: Geostationary Orbit | Geostationary Transfer Orbit | Geosynchronous Transfer Orbit | Low Earth Orbit | Lunar Orbit | Lunar flyby | Mars Orbit | Medium Earth Orbit | Polar Orbit | Suborbital | Sun-Synchronous Orbit | Unknown
Month
Ninth of ten GPS III missions.
02:30 Minute
QZSS (Quasi Zenith Satellite System) is a Japanese satellite navigation system operating from inclined, elliptical geosynchronous orbits to achieve optimal high-elevation visibility in urban canyons and mountainous areas. The navigation system objective is to broadcast GPS-interoperable and augmentation signals as well as original Japanese (QZSS) signals from a three-spacecraft constellation.
The navigation system objective is to broadcast GPS-interoperable and augmentation signals as well as original Japanese (QZSS) signals from a three-spacecraft constellation in inclined, elliptical geosynchronous orbits.
Month
Payload consists of two satellites for Europe's Galileo navigation system.
Month
The European Space Agency (ESA)'s LEO-PNT (Low Earth Orbit Positioning, Navigation and Timing) demonstrator mission will feature a 10-satellite constellation demonstration mission that will assess how a low Earth orbit fleet of satellites can work in combination with the Galileo and EGNOS constellations in higher orbits that provide Europe’s own global navigation system.
This launch will lift 2 “Pathfinder A” satellites built by Thales Alenia Space and GMV to a 510 km altitude Low Earth Orbit.
Month
This is a replacement satellite for the Indian Regional Navigation Satellite System. The constellation will provide India with an alternative to GPS and will be used for military and civilian use. Located at a geosynchronous orbit, the system will be operated by the Indian government.
Year
QZSS (Quasi Zenith Satellite System) is a Japanese satellite navigation system operating from inclined, elliptical geosynchronous orbits to achieve optimal high-elevation visibility in urban canyons and mountainous areas. The navigation system objective is to broadcast GPS-interoperable and augmentation signals as well as original Japanese (QZSS) signals from a three-spacecraft constellation.
The navigation system objective is to broadcast GPS-interoperable and augmentation signals as well as original Japanese (QZSS) signals from a three-spacecraft constellation in inclined, elliptical geosynchronous orbits.
Year
Glonass-K are the third generation of satellite design for GLONASS satellite navigation system. GLONASS is a Russian space-based navigation system comparable to the similar GPS and Galileo systems. This generation improves on accuracy, power consumption and design life. Each satellite is unpressurized and weighs 935 kg, and has an operational lifetime of 10 years.
Year
Tenth of ten GPS III missions.