The Sentinel satellites are designed within the European Commission Copernicus programme, whose aim is to monitor our planet for environmental, social, and economic purposes. The Sentinel-3 series is focused on ocean observation, with further applications also on land and atmosphere. The mission is based on two identical satellites flying on a polar, Sun-synchronous orbit at altitude 815 km, inclination of 98.6° and a repeat cycle of 27 days. The first satellite, Sentinel-3A was launched in February 2016.
Agency | ESA/EUMETSAT |
Launch date | 2016-02-16 |
Mass | 1250 kg |
Repeat cycle | 27 days |
Semi major axis | 7182470 m |
Eccentricity | 0.000309 |
Inclination | 98.62 ° |
Start of phase | 2016-03-01 |
End of phase | active |
Revolutions | 350 |
List of cycles | Link |
Repeat cycle | 27 days |
Semi major axis | 7182470 m |
Eccentricity | 0.000309 |
Inclination | 98.62 ° |
Start of phase | 2016-03-01 |
End of phase | active |
Revolutions | 350 |
List of cycles | Link |
Repeat cycle | 27 days |
Semi major axis | 7182470 m |
Eccentricity | 0.000309 |
Inclination | 98.62 ° |
Start of phase | 2016-03-01 |
End of phase | active |
Revolutions | 350 |
List of cycles | Link |