TerraSAR-X, an imaging radar Earth observation satellite, is a joint venture being carried out under a public-private-partnership between the German Aerospace Center (DLR) and EADS Astrium. The exclusive commercial exploitation rights are held by the geo-information service provider Astrium. TerraSAR-X was launched on 15 June 2007 and has been in operational service since January 2008. With its twin satellite TanDEM-X, launched 21 June 2010, TerraSAR-X acquires the data basis for the WorldDEM, the worldwide and homogeneous DEM available from 2014.
![]() | This article contains content that is written like an advertisement. (October 2013) |
Mission type | Radar imaging |
---|---|
Operator | DLR |
COSPAR ID | 2007-026A ![]() |
SATCAT no. | 31698 |
Mission duration | Elapsed: 15 years, 2 months, 27 days |
Spacecraft properties | |
Manufacturer | EADS Astrium |
Launch mass | 1,230 kg (2,710 lb) |
Start of mission | |
Launch date | 15 June 2007, 02:14 (2007-06-15UTC02:14Z) UTC |
Rocket | Dnepr |
Launch site | Baikonur 109/95 |
Contractor | ISC Kosmotras |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Semi-major axis | 6,886.39 kilometres (4,279.00 mi)[1] |
Eccentricity | 0.0001445[1] |
Perigee altitude | 514 kilometres (319 mi)[1] |
Apogee altitude | 516 kilometres (321 mi)[1] |
Inclination | 97.44 degrees[1] |
Period | 94.79 minutes[1] |
Epoch | 25 January 2015, 02:35:23 UTC[1] |
![]() |
With its phased array synthetic aperture radar (SAR) antenna (X-band wavelength 31 mm, frequency 9.6 GHz), TerraSAR-X provides high-quality radar images of the entire planet from an Earth polar orbit of 514 km altitude. This is selected so that the satellite follows a Sun-synchronous orbit. This specific orbit means that the satellite moves along the Day-Night boundary of the Earth and allows it to present the same face to the Sun: thus, providing the best solar incidence angles to its solar cells for power. TerraSAR-X is designed to carry out its task for five years, independent of weather conditions and illumination, and reliably provides radar images with a resolution of up to 1m.
Features of TerraSAR-X:
TerraSAR-X acquires radar data in the following three main imaging modes:
In addition, the design of TerraSAR-X's SAR antenna allows a variety of polarimetric combinations: single or dual polarization, or full polarimetric data takes.
Depending on the desired application, one of four different processing levels is selected:
TanDEM-X (TerraSAR-X add-on for Digital Elevation Measurements) is a second, similar spacecraft launched successfully on 21 June 2010 from Baikonur Cosmodrome in Kazakhstan. Since October 2010, TerraSAR-X and TanDEM-X have orbited in close formation at distances of only a few hundred metres and record data synchronously.[3] This twin satellite constellation will allow the generation of WorldDEM, the global digital elevation models (DEMs). With higher accuracy, coverage and quality – WorldDEM is a consistent DEM of the Earth's land surface is envisaged to be acquired and generated within three years after launch. Available from 2014, WorldDEM is to feature a vertical accuracy of 2m (relative) and 10m (absolute), within a horizontal raster of approximately 12x12 square meters, slightly varying depending on the geographic latitude.[4]
Radar stands for Radio Detection and Ranging and contains traditionally:
Satellite radar entered use more than fifteen years after optical camera systems did. The resolution is lower than optical imaging, but radar can gather information at any time of the day or night and independent of cloud cover.
Early radar satellite techniques were e.g. the Altimetrie (leveling over the sea), NASA's SEASAT (launched in 1978), regulation of waves/wind or soil data. The military has used radar since the late 1930s and radar satellites at least since 1978.[5]
TerraSAR X will exhibit some technical-industrial novelties. One of these innovations is a kind of zoom shot, with the resolution and scanning field vice versa changeable in a 1:10 relationship, either a larger area to grasp or a small area with the highest possible resolution.
Furthermore, the antenna can be aligned by electronics within an angle range so that the point of view is adjustable. Earlier radar satellites could radiate the antenna only in one direction.
With the adjustable angle radar sensor - along with other course refinements (precession by the earth flattening) - any place on earth can be observed preferentially within 1–3 days.
For a specific point on the Earth's equator, TerraSAR X has a revisit cycle of 11 days. The revisit time decreases towards the poles, e.g. northern Europe has a revisit time of typically 3–4 days.
The ground operating mechanism and controls for the TerraSAR X is developed by the DLR in Oberpfaffenhofen. It consists of Mission Operating Equipment, the Payload Ground Segment and the Instrument Operation and Calibration Segment. At the base of the ground segment lies the German Space Operation Center (GSOC), the German Remote Sensing Datum Center (DFD) as well as Institutes for Methodology of Remote Sensing (MF) and the Institute for High-Frequency Engineering and Radar Systems (HR) which are all part of the DLR.
Applications of the high-resolution TerraSAR-X radar imagery include:
The scientific use of the TerraSAR-X data will be coordinated through the TerraSAR-X Science Service System by the DLR.[10] The new-quality data records, as provided by TerraSAR-X, will offer a vast amount of new research incentives, for instance in ecology, geology, hydrology and oceanography. The smallest movements of the Earth's surface (plate tectonics, volcanism, earthquake) are further scientific fields of application.
In order to ensure the commercial success of the mission, EADS Astrium founded its 100% subsidiary Infoterra in 2001; the company being responsible for establishing a commercial market for TerraSAR-X data as well as TerraSAR-X-based geo-information products and services.
Radars on the Space Shuttle:
(the TerraSAR-X authors were involved in SRL and SRTM missions)
Orbital meteorological and remote sensing systems | |||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|
Concepts |
| ||||||||||
Current projects |
| ||||||||||
Former projects |
|
← 2006 · Orbital launches in 2007 · 2008 → | |
---|---|
January | |
February | Beidou-1D | THEMIS A · THEMIS B · THEMIS C · THEMIS D · THEMIS E | IGS Radar 2 · IGS Optical 3V |
March | |
April | Soyuz TMA-10 | Anik F3 | Hai Yang 1B | Compass-M1 | EgyptSat 1 · Saudisat-3 · SaudiComsat-3 · SaudiComsat-4 · SaudiComsat-5 · SaudiComsat-6 · SaudiComsat-7 · CP-3 · CP-4 · CAPE-1 · Libertad 1 · AeroCube 2 · CSTB-1 · MAST | AGILE · AAM | NFIRE | AIM |
May | Astra 1L · Galaxy 17 | Progress M-60 | NigComSat-1 | Yaogan 2 · Zheda PiXing 1 | Globalstar 65 · Globalstar 69 · Globalstar 71 · Globalstar 72 | Sinosat-3 |
June | Kosmos 2427 | COSMO-1 | STS-117 (ITS S3/4) | Ofek-7 | TerraSAR-X | USA-194 | Genesis II | Kosmos 2428 |
July | SAR-Lupe 2 | Zhongxing 6B | DirecTV-10 |
August | |
September | INSAT-4CR | JCSAT-11 | Kosmos 2429 | Kaguya (Okina · Ouna) | Foton-M No.3 · YES2 | WorldView-1 | CBERS-2B | Dawn |
October | Intelsat 11 · Optus D2 | Soyuz TMA-11 | USA-195 | USA-196 | Globalstar 66 · Globalstar 67 · Globalstar 78 · Globalstar 70 | Kosmos 2430 | STS-120 (Harmony) | Chang'e 1 | Kosmos 2431 · Kosmos 2432 · Kosmos 2433 |
November | |
December | Globus-1M No.11L | COSMO-2 | USA-198 | Radarsat-2 | USA-199 | Horizons-2 · Rascom-QAF 1 | Progress M-62 | Kosmos 2434 · Kosmos 2435 · Kosmos 2436 |
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets. |