The space segment of the system includes four identical medium-sized 1,700 kg (3,700 lb) satellites called COSMO-SkyMed (or COSMO) 1, 2, 3, 4, equipped with synthetic-aperture radar (SAR) sensors with global coverage of the planet.[4] Observations of an area of interest can be repeated several times a day in all-weather conditions. The imagery is applied to defense and security assurance in Italy and other countries, seismic hazard analysis, environmental disaster monitoring, and agricultural mapping.[5]
COSMO-SkyMed first generation
The four satellites are in Sun-synchronouspolar orbits with a 97.90° inclination at a nominal altitude of 619 km (385 mi) and an orbital period of 97.20 minutes. The local time ascending node at the equator is 06:00. The operating life of each satellite is estimated to be 5 years. Each satellite repeats the same ground track every 16 days. They cross the equator at approximately 06:00 and 18:00 local-time each day and can image any point twice each day. The satellites are phased in the same orbital plane, with COSMO-SkyMed's 1, 3, and 2 at 90° intervals followed by COSMO-SkyMed 4 at 67.5° after COSMO-SkyMed 2. The offset of satellite 4 allows a one-day interferometry mode for elevation information.[6] The Sun-synchronous orbit (SSO) is used due to power (Electrical Power Subsystem) and revisit time requirements.
The radar antenna is a phased array that is 1.4 × 5.7 m (4 ft 7 in × 18 ft 8 in). The system is capable of both single- and dual-polarization collection. The center frequency is 9.6 GHz with a maximum radar bandwidth of 400 MHz.[7]
List of launches
United Launch Alliance provided launch services for the satellites with their Delta II 7420-10C launch vehicles from Vandenberg Air Force Base.[8] Satellite processing for the first two satellites was handled by the Astrotech Space Operations subsidiary of SPACEHAB.[5] The first satellite COSMO-1 (COSPAR 2007-023A) was launched at 02:34:00 UTC on 8 June 2007.[9] COSMO-2 (COSPAR 2007-059A) was launched at 02:31:42 UTC on 9 December 2007,[10] the launch having been delayed from 6 December 2007 due to bad weather, and problems with the rocket's cork insulation. COSMO-3 (COSPAR 2008-054A) launched at 02:28 UTC on 25 October 2008. COSMO-4 (COSPAR 2010-060A) launched on 6 November 2010, at 02:20 UTC.[11]
The governments of Argentina and France are involved respectively in the civil and military segments of the system.
SAR capabilities
The COSMO-SkyMed satellites have three basic types of imaging modes:
Spotlight, a high-resolution mode collected over a small area by steering the radar beam slightly fore-to-aft during the collection period
Stripmap, a medium-resolution mode collected over long, continuous swaths in which the beam is pointed broadside to the satellite track
ScanSAR, a low-resolution mode that creates extra-wide swaths by collecting short segments at different ranges and then mosaicking them together
There are two Spotlight modes:
SPOTLIGHT1, which is a military-only mode, and
SPOTLIGHT2, which provides a resolution of 1 m (3 ft 3 in) over a 10 × 10 km (6.2 × 6.2 mi) area. Spotlight polarization is limited to either HH or VV
There are two Stripmap modes:
HIMAGE, which provides a resolution of between 3 and 5 m (9.8 and 16.4 ft) over a swath of 40 km (25 mi), and
PINGPONG, which collects dual-polarization data at 15 m (49 ft) resolution over a swath of 30 km (19 mi). The dual-polarization data can consist of any two polarizations (HH, VV, VH, HV), and it is non-coherent, as it is collected in "pulse groups" that alternate from one polarization to the other.
There are two ScanSAR modes:
WIDEREGION, which provides 30 m (98 ft) resolution data over a swath of 100 km (62 mi), and
HUGEREGION, which provides 100 m (330 ft) resolution data over a swath of 200 km (120 mi).
The system is sized to collect up to 450 images per satellite per day.[12]
Overview of Damage Proxy Map from COSMO-SkyMed data
e-GEOS, S.p.A., a joint venture between European spaceflight services company Telespazio (80%) and the Italian Space Agency (ASI) (20%), has the exclusive worldwide commercial rights to sell COSMO-SkyMed data and products.[13][12]
Flares
The COSMO-SkyMed satellites are lesser-known deliverers of satellite flares, sometimes approaching magnitude −3. Flares come mainly from SAR-panels of the satellites. Although overshadowed by the Iridium satellites, the flares are often long-lasting, with the satellites traversing much of the sky at brighter-than-average magnitudes.
COSMO-SkyMed second generation (CSG)
To replace the first COSMO-SkyMed constellation, the Italian Space Agency is developing the COSMO-SkyMed second generation constellation. The 2nd generation constellation has the same function of radar-based Earth observation with particular focus on the Mediterranean area as the 1st generation. Like the 1st generation, the 2nd generation also consists of 4 satellites, CSG-1, CSG-2, CSG-3 and CSG-4. The satellites are improved versions of the first generation satellites. Also the radar payload CSG-SAR (COSMO-SkyMed Second Generation Synthetic Aperture Radar) is an improved version of the first generation X-band SAR payload. Furthermore, the 2nd generation satellites will operate in the same orbit (indeed, in the same orbital plane) as the first generation satellites. The 2nd generation satellites slightly outweigh the first generation satellites at 2,205 kg (4,861 lb) of mass.[14]
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
