Sentinel-1A

Sentinel-1A
Model of a Sentinel-1 satellite (radar antenna missing)
Mission typeEarth observation
OperatorESA
COSPAR ID2014-016A Edit this at Wikidata
SATCAT no.39634
WebsiteSentinel-1 (ESA)
Mission durationPlanned: 7 years[1]
Elapsed: 10 years, 5 months, 15 days
Spacecraft properties
Spacecraft typeSentinel-1
BusPrima
ManufacturerThales Alenia Space
EADS Astrium
Launch mass2,300 kg (5,100 lb)
Dry mass2,170 kg (4,780 lb)
Dimensions3.4 m × 1.3 m (11.2 ft × 4.3 ft)
Power5900 watts
Start of mission
Launch date3 April 2014, 21:02:31 (2014-04-03UTC21:02:31) UTC[2]
RocketSoyuz-STA/Fregat
Launch siteKourou ELS
ContractorArianespace
Orbital parameters
Reference systemGeocentric
RegimeSun-synchronous
Apogee altitude693 km (431 mi)[3]
Inclination98.18 degrees
Period98.6 minutes
Repeat interval12 days
Epochplanned
Transponders
BandS Band (TT&C support)
X Band and Optical laser through EDRS (data acquisition)
Bandwidth64 kbit/s upload (S Band)
128 kbit/s – 2 Mbit/s down (S Band)
520 Mbit/s down (X Band/Optical)

Sentinel-1A is a European radar imaging satellite launched in 2014. It is the first Sentinel-1 satellite launched as part of the European Union's Copernicus programme. The satellite carries a C-band Synthetic Aperture Radar which will provide images in all light and weather conditions. It analyzes many phenomena occurring on Earth, from detecting and tracking oil spills and mapping sea ice to monitoring movement in land surfaces and mapping changes in the way land is used.

  1. ^ "Sentinel-1 facts & figures" (PDF). ESA. 2013. Retrieved 5 March 2014.
  2. ^ "Earth Online – Sentinel 1". ESA. Archived from the original on 2 March 2014. Retrieved 5 March 2014.
  3. ^ "Copernicus: Sentinel-1 — The SAR Imaging Constellation for Land and Ocean Services". ESA eoPortal. Archived from the original on 2 March 2014. Retrieved 5 March 2014.