Division 3.2.1 Space Segment general description
United Kingdom
The dedicated Sentinel missions shall carry a range of technologies, including radar and multispectral imaging instruments for land, ocean and atmospheric monitoring. They shall be developed by ESA and organised into six different mission families.
Sentinel-1 mission: shall comprise a constellation of at least two polar-orbiting satellites to reach Full Operational Capacity (FOC), operating day and night performing C-band synthetic aperture radar imaging, enabling them to acquire imagery regardless of the weather;
Sentinel-2 mission: shall comprise a constellation of at least two two polar-orbiting satellites aiming to monitor variability in land surface conditions supporting the monitoring of changes to vegetation within the growing season;
Sentinel-3 mission: shall comprise a constellation of at least two polar-orbiting satellites with the objective to monitor oceans and land masses globally. Sentinel-3 partim marine shall measure sea surface topography, sea surface temperature, and ocean surface colour to support ocean forecasting systems, environmental monitoring and climate monitoring. Sentinel-3 partim land shall measure land and inland water surface height, land surface temperature and land surface colour;
Sentinel-4 mission: Sentinel-4 shall monitor key air quality trace gases and aerosols over Europe in support of the Copernicus Atmosphere Monitoring Service (CAMS) at high spatial resolution and with a fast revisit time. Sentinel-4 shall be implemented as part of the Geostationary EUMETSAT Meteosat Third Generation Satellite System. The Sentinel-4 instruments shall be hosted on the EUMETSAT satellites MTG-S-1 (Sentinel-4A) and MTG-S-2 (Sentinel-4B), with an expected 15,5 years of operations for both satellites combined;
Sentinel-5 mission: Sentinel-5 shall provide accurate measurements of key atmospheric constituents such as ozone, nitrogen dioxide, sulphur dioxide, carbon monoxide, methane, formaldehyde, and aerosol properties. Sentinel-5 shall be implemented as part of the EUMETSAT Polar System of Second Generation (EPS-SG). The Sentinel-5 instruments shall be hosted on the EUMETSAT satellites METOP-SG-A-1, METOP-SG-A-2, METOP-SG-A-3 (each with a design lifetime of 7,5 years and hosting Sentinel-5A, -5B, -5C respectively). Sentinel-5pf1 shall be the precursor mission to Sentinel-5;
Sentinel-6 mission: shall be a radar altimeter mission, with the objective of providing high-precision measurements of global sea-level as a reference altimetry mission. Sentinel-6 shall consist of 2 units (A and B, each with a design lifetime of 5 years) covering 10 years of observations.
Sentinel-1, Sentinel-2 and Sentinel-3 shall consist each of 4 satellites, whereby 2 units are needed to reach Full Operational Capacity (FOC) and 2 units shall ensure recurrent observation capacity after the end-of-life of the first 2 units.
The operations of Jason-3 f2 shall be included in the Copernicus Space Component to provide continuity of observations between Jason-2 and Sentinel-6 as a reference altimetry mission.
The characteristics of the Copernicus dedicated missions shall be as specified in Table 2.
Table 2
Copernicus Dedicated missions characteristics
| The period of operations may change depending upon the actual life time of the individual satellite units and evaluation of programmatic options. | |||||
| Abbreviations: VIS = Visual Range Bands; SWIR = Short Wave Infrared; MWIR = Mid-Wave Infrared; TIR = Thermal Infrared. | |||||
| Sentinel Mission | Main Characteristic and purpose | Number of Units | Payloads | Satellite orbit | Approximate Period of operationsf3 |
|---|---|---|---|---|---|
| Sentinel-1 | RADAR Mission | 4 units (A, B, C, D), two units are flying in parallel for full capacity | C-Band SAR Payload with centre frequency of 5,405 GHz (4 polarisations) and 4 modes:
| Sun-Synchronous orbit at approximately 693 km | A, B: 2014 – 2022 C, D: 2022-2030 |
| Sentinel-2 | High Resolution optical mission for land imaging | 4 units (A, B, C, D), two units are flying in parallel for full capacity | — MSI — Multi Spectral Imager with 13 multispectral channels between 400 nm and 2 300 nm, spectral resolution between 1 nm and 180 nm and spatial resolutions of 10 m, 20 m and 60 m. Includes an Optical Communication Payload for mission data relay through EDRS. | Sun-Synchronous orbit at approximately 786 km | A, B: 2015 – 2023 C, D: 2023-2030 |
| Sentinel-3 | Global Ocean and Land Imaging | 4 units (A, B, C, D), two units are flying in parallel for full capacity |
| Sun-Synchronous orbit at approximately 814,5 km | A, B: 2016 – 2023 C, D: 2023-2030 |
| Sentinel-4 | Atmospheric monitoring | 2 instruments (A, B), on board consecutive Meteosat Third Generation – Sounder satellites | The Sentinel-4 instrument is a high-resolution imaging spectrometer (spatial resolution of 8 × 8 km) covering three wavelength bands:
| On board Meteosat Third Generation Satellites in geostationary orbit at approximately 35 786 km. Coverage of Europe and North Africa with a repeat cycle of about 60 minutes | 2022 - 2040 |
| Sentinel-5 | Atmospheric monitoring | 3 units (A, B, C), on board consecutive METOP Second Generation – A satellites | The Sentinel-5 UVNS instrument is a high resolution spectrometer (spatial resolution about 7 km), covering the following wavelength bands:
| Part of the EUMETSAT Polar System of Second Generation (EPS-SG) at approximately 817 km | 2022-2040 |
| Sentinel-5p | Atmospheric monitoring | Precursor satellite for Sentinel-5 | — TROPOMI — TROPOspheric Monitoring Instrument with 4 channels in the following spectral ranges: 270-500 nm, 675-775 nm, 2 305-2 385 nm and spatial resolution of 7 × 7 km | Sun-Synchronous orbit at approximately 824 km | 2017 - 2024 |
| Sentinel-6 | High Precision Ocean Altimetry | 2 units (A, B) |
| Non-Sun-synchronous at approximately 1 336 km | A: 2020 – 2025 B: 2025 - 2030 |
Annotations
Footnotes
- f1
-
The Sentinel-5 Precursor (Sentinel-5p) mission is a joint initiative between ESA and the Kingdom of the Netherlands.
- f2
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Jason-3 is the result from the long-standing cooperation between EUMETSAT, NOAA, CNES and NASA. It is a High Precision Ocean Altimetry Mission that provides continuity between Jason-2 and Sentinel-6 and is operational since 2016 with an envisaged lifetime of 5 years.
- f3
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The period of operations may change depending upon the actual life time of the individual satellite units and evaluation of programmatic options.
- f4
-
Abbreviations: VIS = Visual Range Bands; SWIR = Short Wave Infrared; MWIR = Mid-Wave Infrared; TIR = Thermal Infrared.