Strela-1M
ISS Reshetnev
The Strela-1M is a communication and broadcasting satellite developed by ISS Reshetnev, designed for low circular orbit operations.
Key figurescomparable across the catalogue
- Mass
- 70 kg
- Design life
- 0.5 years
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- ADCS type
- unoriented
- EPS power
- 8 W
- Mass
- 70 kg
- Lifetime
- 6-9 months
- Orbit
- Low circular
- Orbit height
- 1000 km
- Launch vehicle
- Kosmos-3M carrier rocket
- Cosmodromes
- Plesetsk
- First launch date
- 25 April 1970
About
The Strela-1M is a satellite developed by ISS Reshetnev for communications and broadcasting purposes. It operates in a low circular orbit at a height of 1000 km. The satellite has an unoriented attitude determination and control system (ADCS) and an electrical power system (EPS) providing 8 W of power. With a mass of 70 kg, the Strela-1M is designed for a lifetime of 6-9 months. Its launch vehicle is the Kosmos-3M carrier rocket, typically launched from the Plesetsk Cosmodrome. The first launch of a Strela-1M satellite was on April 25, 1970.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.