![]() Image of Kanopus-V | |
Mission type | Earth observation |
---|---|
Operator | Roscosmos |
Mission duration | 5 years |
Spacecraft properties | |
Manufacturer | NPP VNIIEM |
Launch mass | 473 kg (1,043 lb) |
Start of mission | |
Launch date | 22 July 2012 (Kanopus-V №1 & BKA) 05 December 2015 (Kanopus-ST №1/Kosmos 2511) 14 July 2017 (Kanopus-V IK №1) 01 February 2018 (Kanopus-V №3 & 4) 27 December 2018 (Kanopus-V №5 & 6) |
Rocket | Soyuz-FG/Fregat Soyuz-2.1v/Volga Soyuz-2.1a/Fregat-M |
Launch site | Baikonur,Site 31/6 Plesetsk, Site 43/4 Vostochny, Site 1S |
Contractor | Roscosmos |
Orbital parameters | |
Reference system | Geocentric orbit |
Regime | Sun-synchronous orbit |
Kanopus also known as Canopus, is a series of Russian Earth Observation satellite developed and operated by Roscosmos, primarily through the Research and Production Corporation VNIIEM. The program is designed for real-time monitoring of natural and man-made disasters, environmental changes, agriculture, cartography, and resource management. The Kanopus satellites operate in Sun-synchronous orbits at approximately 500–510 km altitude, offering high-resolution imaging and frequent revisits. The program emphasizes cost-effective, modular designs using the Kanopus bus platform, with contributions from international partners such as Surrey Satellite Technology Ltd (SSTL) of the United Kingdom for avionics and software. [1]
The Kanopus program was initiated in the early 2000s to enhance Russia's domestic Earth observation capabilities. The initial design for Kanopus-V (Canopus-B) was proposed by 2008, with a planned mass of 350 kg, which increased to 473 kg by 2011 due to design refinements. Payload capacity was adjusted from 150 kg to 108 kg, power output from 350 W to 300 W, and the operational lifespan reduced from 7 to 5 years. The satellites were configured for a Sun-synchronous orbit at 510–540 km with a 97.4–97.5° inclination to optimize illumination.
Development faced delays due to a 2007 agreement with Belarus to co-develop the BKA satellite, a near-identical copy of Kanopus-V, as a replacement for Belarus's lost BelKA spacecraft. This led to a joint launch in 2012. The program has since expanded to include infrared-capable variants and proposals for radar (Kanopus-R) and cartography (Kanopus-K) models, though some, like Kanopus-VM, were canceled before 2019. As of 2025, the Kanopus constellation supports Russian federal agencies for applications such as forest fire detection, earthquake prediction, and coastal monitoring. [2]
The Kanopus family of satellites have many variants for several applications:
The baseline model, designed for high-resolution panchromatic and multispectral Earth observation. It features a 2.1 m resolution panchromatic camera (20 km swath) and a 10.5 m resolution multispectral camera (41 km swath). Applications include disaster monitoring, urban planning, and agriculture. [3] [4]
Kanopus-V-IK is the infrared-capable variant modified from Kanopus-V №2 satellite, equipped for thermal imaging. It can detect fire sources as small as 5x5 m over a 2,000 km area. [5] [6]
BKA is the Belarusian variant, nearly identical to Kanopus-V, It is developed under a Russia-Belarus agreement. It is operated by Belarus for national Earth observation purposes. [7]
Kanopus-ST is an experimental military variant launched in 2015 on a Soyuz-2.1v rocket for submarine tracking and defense-related tests. Details remain limited due to its classified nature. [8]
Next-generation models with expanded coverage (up to 100 km swath) and improved infrared sensors, planned for enhanced disaster response by 2025–2026.
Other concepts, such as Kanopus-D (detailed observation) and Zond-PP (related platform), have been tested as secondary payloads. [9]
Name | SATCAT | Launch date (UTC) | Launch vehicle | Orbital apsis | Inclination | Period (min) | Status |
---|---|---|---|---|---|---|---|
Kanopus-V №1 [10] | 22 July 2012 | Soyuz-FG/Fregat | Operational | ||||
BKA №1 | Operational | ||||||
Kanopus-ST (Kosmos 2511) [11] [12] | 05 December 2015 14:08 | Soyuz-2.1v/Volga | Failed to Separate | ||||
Kanopus-V-IK (Kanopus-V №2) [13] [14] | 14 July 2017 | Soyuz-2.1a/Fregat | Operational | ||||
Kanopus-V №3 [15] [16] | 01 February 2018 | Soyuz-2.1a/Fregat-M | Operational | ||||
Kanopus-V №4 | Operational | ||||||
Kanopus-V №5 [17] [18] | 27 December 2018 | Operational | |||||
Kanopus-V №6 | Operational | ||||||
Kanopus-V №7 | 2025 | Planned | |||||
Kanopus-V №8 | Planned | ||||||