| |
| Mission type | Space weather |
|---|---|
| Operator | |
| Spacecraft properties | |
| Bus | HP-IOT |
| Manufacturer | |
| Start of mission | |
| Launch date | 2027 (planned) |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Sun-synchronous |
| Altitude | Between 500 and 600 km |
SWING (Space Weather Ionosphere Nanosat Generation) is a future space weather mission for monitoring Earth's ionosphere, [1] under development by the European Space Agency's Space Safety Programme (S2P). [2] SWING will be the agency's first space weather nanosatellite and the first part of the S2P's Distributed Space Weather Sensor System (D3S). [3] [4] It is expected to launch in 2027. [5]
The prime contractor of the mission is the French company Hemeria, [2] [6] [7] [8] [9] while Syntony GNSS (France) will provide the satellite's GNSS receiver [10] and Planetek (Italy) will develop the mission operations center. [11] The satellite's design is based on Hemeria's HP-IOT nanosatellite platform. [12] [13]
The satellites's payload consists of four instruments: [12]