TARKOT Block BII: Difference between revisions
Jump to navigation
Jump to search
No edit summary |
No edit summary |
||
(10 intermediate revisions by 2 users not shown) | |||
Line 14: | Line 14: | ||
| orbits = {{wp|Semi-synchronous orbit|Semi-synchronous}} {{wp|Medium Earth orbit|MEO}} | | orbits = {{wp|Semi-synchronous orbit|Semi-synchronous}} {{wp|Medium Earth orbit|MEO}} | ||
| operator = {{flag|Cordomonivence}} <br> [[Costak]] <br> [[Adrinian]] <br> | | operator = {{flag|Cordomonivence}} <br> [[Costak]] <br> [[Adrinian]] <br> {{flag|Greater Penguinia}} <br> TBA | ||
| lifetime = 15 years (planned) | | lifetime = 15 years (planned) | ||
| derivedfrom = TARKOT Block BI | | derivedfrom = TARKOT Block BI | ||
Line 22: | Line 22: | ||
| status = In production | | status = In production | ||
| built = 24 | | built = 24 | ||
| orders = 6 | | orders = 6 | ||
| launched = 24 | | launched = 24 | ||
| operational = 24 | | operational = 24 | ||
| retired = | | retired = | ||
| failed = | | failed = | ||
| lost = | | lost = | ||
| first = 18 May 2015 | | first = 18 May 2015 | ||
| last = 1 August 2023 | | last = 1 August 2023 | ||
| lastretired = | | lastretired = | ||
Line 41: | Line 41: | ||
| dimensions = | | dimensions = | ||
}} | }} | ||
'''TARKOT Block BII''' is the latest satellite design of the Cordobez [[Global Navigation Satellite System TARKOT]] {{wp|satellite navigation system}}.Developed by [[Munkers Fatter]] and first launched on 18 May 2015 its a substantial improvement of the previous [[TARKOT Block BI]] generation of satellites,having a longer lifespan,better accuracy and improved security. | '''TARKOT Block BII''' is the latest satellite design of the Cordobez [[Global Navigation Satellite System TARKOT]] {{wp|satellite navigation system}}.Developed by [[Munkers Fatter]] and first launched on 18 May 2015 its a substantial improvement of the previous [[TARKOT Block BI]] generation of satellites,having a longer lifespan,better accuracy and improved security. |
Latest revision as of 21:00, 12 April 2024
This article is incomplete because it is pending further input from participants, or it is a work-in-progress by one author. Please comment on this article's talk page to share your input, comments and questions. Note: To contribute to this article, you may need to seek help from the author(s) of this page. |
Manufacturer | Munkers Fatter | ||
---|---|---|---|
Country of origin | Cordomonivence | ||
Operator | Cordomonivence Costak Adrinian Greater Penguinia TBA | ||
Applications | Navigation satellite | ||
Specifications | |||
Bus | K2-4000 | ||
Design life | 15 years (planned) | ||
Launch mass | 1,780 kg (3,920 lb) | ||
Dry mass | 1,080 kg (2,380 lb) | ||
Power | 2383 watts (end of life) | ||
Batteries | Nickel–hydrogen battery | ||
Regime | Semi-synchronous MEO | ||
Production | |||
Status | In production | ||
Built | 24 | ||
On order | 6 | ||
Launched | 24 | ||
Operational | 24 | ||
First launch | 18 May 2015 | ||
Last launch | 1 August 2023 | ||
Related spacecraft | |||
Derived from | TARKOT Block BI | ||
|
TARKOT Block BII is the latest satellite design of the Cordobez Global Navigation Satellite System TARKOT satellite navigation system.Developed by Munkers Fatter and first launched on 18 May 2015 its a substantial improvement of the previous TARKOT Block BI generation of satellites,having a longer lifespan,better accuracy and improved security.