Ionosfera-M
| Mission type | Earth observation |
|---|---|
| Operator | Roscosmos |
| Mission duration | 8 years (planned) |
| Spacecraft properties | |
| Manufacturer | NPP VNIIEM |
| Launch mass | 430 kg (950 lb) |
| Start of mission | |
| Launch date | 04 November 2024 (Ionosfera-M №1&2) 25 July 2025 (Ionosfera-M №3&4) |
| Rocket | Soyuz-2.1b/Fregat-M |
| Launch site | Vostochny, Site 1S |
| Contractor | Roscosmos |
| Orbital parameters | |
| Reference system | Geocentric orbit |
| Regime | Sun-synchronous orbit |
Project Ionozond | |
Ionosfera-M is a Constellation of four Ionospheric and Magnetospheric research Earth observation satellite system developed by Roscosmos for Project Ionozond.