SESAT
ISS Reshetnev
SESAT is a geostationary communications satellite developed by ISS Reshetnev, launched on April 18, 2000.
Key figurescomparable across the catalogue
- Mass
- 2,572 kg
- Design life
- 10 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
- active
- EPS power
- 5300 W
- Mass
- 2572 kg
- Lifetime
- 10 years
- Orbit
- GEO
- Orbit height
- 36000 km
- Launch vehicle
- Proton-K carrier rocket and DM upper stage
- Cosmodromes
- Baikonur
- First launch date
- 18 April 2000
About
The SESAT satellite is a communications and broadcasting spacecraft developed by ISS Reshetnev. It operates in Geostationary Earth Orbit (GEO) at an altitude of 36,000 km. The satellite has an active Attitude Determination and Control System (ADCS) and an Electrical Power System (EPS) with a power output of 5300 W. With a mass of 2572 kg, SESAT is designed for a lifetime of 10 years. Its launch was carried out using a Proton-K carrier rocket and a DM upper stage from the Baikonur Cosmodrome, with the first launch date recorded as April 18, 2000. This satellite is part of ISS Reshetnev’s extensive portfolio of communications and broadcasting spacecraft.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.