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16 federal space agency of russia

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GeoMedeelel
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The Research Center for Earth Operative Monitoring (NTs OMZ) acts as the Russian Federal Space Agency’s ground segment for acquiring, processing, and disseminating data from Russian and foreign remote sensing spacecraft. The NTs OMZ performs planning, acquisition, processing, archiving, and dissemination of data from ROSKOSMOS spacecraft and provides remote sensing data and value-added products to domestic and international customers. The NTs OMZ maintains Earth observation spacecraft, processes petabytes of remote sensing data using advanced technologies, and offers a variety of data products and services to support applications in resource management, environmental monitoring, emergency response, and more

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FEDERAL SPACE AGENCY OF RUSSIA RESEARCH CENTER FOR EARTH OPERATIVE MONITORING FASILITIES OF REMOUTE SENSING SPACECRAFT OPERATOR Address: 51, corp. 25 Dekabristov St., Moscow, 127490, Russia, NTs OMZ Phone:(495) 925-04-19, Fax: (495) 404-77-45, E-mail:ntsomz@ntsomz.ru, Internet:www.ntsomz.ru 1
Operator of russian remote sensing spacecrafts The Research Center for Earth Operative Monitoring (NTs OMZ) acts as the Russian Federal Space Agency’s ground segment for space data planning, acquisition, processing, and dissemination. The NTs OMZ performs an entire technological cycle of planning, acquisition, recording, processing, archiving, storing, and dissemination of data from the ROSKOSMOS’s remote sensing spacecraft as well as from foreign satellites within the framework of concluded agreements and contracts. The NTS OMZ is equipped with the antenna systems and uses modern high technologies for space data processing and archiving, maintains a unified E-catalog and the ROSKOSMOS’s archive of the remote sensing data, provides consumers with a remote access to space data. The modern technological and methodological base allows for the foreign remote sensing spacecraft and their data to be dealt with. The NTs OMZ completing orders for operational imaging of the Earth’s surface and having a large fund of remote sensing data, offers customers remote sensing data of various spatial resolution from both the Russian and foreign satellites as well as value-added processing of the data and implementation of thematic projects. 2
Main Tasks of Center for Operational Acquisition, Processing and Dissemination of Space Data on Earth • Acts as a parent organization of the Russian Space Agency on remote sensing space system operation to the benefit of socio-economic development of the Russian Federation and international collaboration; • Acts as an Operator for exploitation and end use of the Russian remote sensing system and provision of consumers with remote sensing data; • Provides and conducts in-flight tests of onboard scientific and information equipment; • Makes plans of imaging, provides acquisition, recording, processing, and dissemination of remotely-sensed data from the Russian spacecraft; • Provides federal, regional, departmental and commercial consumers with remote sensing data; • Creates and maintains E-catalog and fund of remote sensing data and value-added products; • Makes co-ordination and scientific and methodical supervision of the Russian and foreign centers and stations of data acquisition, processing and archiving from the Russian spacecraft; • Interacts with appropriate foreign organization on remote sensing data acquisition, processing, archiving and distributing; • Develops scientific and applied projects including international ones, to derive new data products from space observations; • Contributes to international and scientific and technical cooperation in the context of intergovernmental agreements, and performs an international exchange of space data in accordance with concluded agreements and contracts. 3
RESURS- DK1 MISSION Multi-spectral high resolution remote sensing of the Earth’s surface designed for acquisition of high quality imagery as in near real-time as on-line to be delivered via radio link. Spacecraft and orbit parameters: Spacecraft mass - 6570 kg Payload mass - 1200 kg Altitude - H=360-604 km Inclination - 70,0° RESURS- DK1 Modules and Blocks 4
RESURS- DK1 SPECIFICATIONS Remote-sensing instrument features: • Multispectral capabilities - 3 spectral bands. • Spectral bands: • 1-3 spectral bands to be recorded simultaneously; • wavelengths are 0,58-0,8 micrometers (panchromatic mode), 0,5-0,6, 0,6-0,7, 0,7-0,8 (narrow bands in multispectral mode). • Spatial resolution – 1,0m in panchromatic mode and 2,0-3,0 m in narrow bands at nadir, 350 km altitude, 30º sun elevation angle over local horizon. • Swath width at the altitude of 350 km at nadir is 28,3 km, 57km at ±45º incidence angle (roll). • Field of view at the altitude of 350 km is 700 km (±45º inclination). • Position accuracy by orbital data is 100 m. • Revisiting frequency at nadir is 3-6 days. • Observation time for stripes - from 2 to 300 s. • Maximum technical capacity – 1 mln. sq. km per day. 5
RESURS- DK1 DATA ACQUSITION MODES 6
RESURS- DK1 Applications • Data supply for resource management and economical activity (inventory of natural resources, topographic and thematic mapping); • Monitoring of pollution sources of the atmosphere, water and soil with the view of providing Federal and regional environmental authorities with the relevant information to make management decisions; • On-line monitoring of man-caused and natural emergencies for the purpose of effective planning and timely performing of measures to eliminate damages; • Supplying home and foreign consumers on a commercial basis; • Research activities (PAMELA Experiment — space exploration to search and study antimatters: antiprotons, positrons, nuclear and electronic components in primary space radiation). 7
Comparative Data over Areas Imaged from Multiple Remote Sensing Spacecraft OrbView - 3 8 x 8 km 8 x 8 км Lм=0,6 м IKONOS 11 x 11 km 11 x 11км Lм=1 м SPOT 60 x 60 km 60 x 60км Lм=2,5 м RESURS RESURS - DK1 28 x 28 km 28 x 28км Lм=1 м 8
KANOPUS-V Space System Designed for Operational Monitoring of Anthropogenic and Natural Emergencies Mission Purpose Panchromatic and multi-spectral imaging of the Earth Recording of abnormal physical phenomena for earthquake prediction Spacecraft mass - 350kg Payload mass - 147kg Altitude - H=510-600km Inclination (ССО) - 98° Lifetime – 7 years Launch date - 4th quarter of 2009 KANOPUS-V Modules and Blocks 9
KANOPUS-V Main Characteristics : • Multi-spectral capabilities - 4 spectral bands; • Spectral bands: • 1-4 spectral bands designed for simultaneous recording; • Wavelength 0.52-0.85 µm (panchromatic mode), 0.54-0.6, 0.63-0.69, 0.69-0.72, 0.75-0.86 µm (narrow ranges in multi-spectral mode); • Spatial resolution – 2.7m in panchromatic mode and 12.0m in narrow ranges at nadir from 510-km altitude; • Field of view at altitude of 510km at nadir – more than 20.0km; • Swath width at altitude of 510km - 1020km (angle of roll ±45º); • Image repeat possibility at nadir (at the equator) – 5 days; • Observing time along the route – up to 350s; • Maximal performance – 500 000 sq. km per day. 10
KANOPUS-V Main Applications • Monitoring of man-made and natural emergencies including natural hydrometeorological disasters; • Detection of forest fire seats, large pollutant emissions; •Monitoring of agricultural activity, natural resources (including water and coastal resources); • Land use; • Operational observation of specified areas of the earth’s surface; • Recording of abnormal physical phenomena in the atmosphere, ionosphere, magnetosphere, and at the Earth’s surface in an effort to predict earthquakes. 11
METEOR-M №1 Spacecraft SEVERYANIN-M On-board Radar Complex (BRLK) Module for Atmospheric Temperature and Humidity Sounding (MTVZA) Meteorological Multi-Band Scanning Device (MSU-MR) Decimetric Radio Link Centimetric Radio Link Multi-Band Imagery Complex Data Collection and for Ecological Heliogeophysical Equipment Transmission System monitoring (KMSS) (GGAK) (SSPD) 12
METEOR-M SPACE SYSTEM Mission Purpose - Acquisition of multiband images Spacecraft mass - 3000kg including radar ones and Orbital altitude - H=830.00km measurements of the ―Earth’s surface – Atmosphere‖ system Inclination (ССО) - 98.85° outgoing radiation over various Orbital period - 101.3min regions of the energy spectrum in terms of absolute radiant qualities; Lifetime - 5 years - Heliogeophysical data acquisition; - Collection and transmission of data Launch date - 2nd quarter of 2009 from automatic data collection platforms (DCP) of different types (ground-based, ice, drifting) deployed in any region of the Earth (including the polar regions). 13
METEOR-M Spacecraft Main Characteristics : MSU-MR: KMSS: - Swath width – 2800km; - Swath width when two cameras operate - Spatial resolution on ground -1000m; simultaneously - 1000-1200km; - Spectral band number – 6; - Resolution – 70m; - Rated values of spectral bands - 0.5-0.7; 0.7-1,1; -Spectral band number - 4; 1.6-1.8; - Rated values of spectral bands - 0.45-0.50; 3.5-4.1; 10.5-11.5; 11.5-12.5µm; 0.535-0.575; 0.63-0.68; 0.76-0,9 µm. - Range of radiation temperatures measured 213-313 °К. MTVZA: BRLK: - Swath width – 1500km; - Swath width – 600km; - Channel number - 26; - Linear resolution on ground - Spatial resolution - 16 – 198km; - 400 – 650m (moderate resolution mode) - Vertical resolution - 4 – 5km; - 800 – 1300m (low resolution mode); - Operating frequency range – 18.7 – 183.31 - Wavelength of sounding pulse - 3.12cm . GHz. 14
RESURS-P: Mission Purpose The RESURS-P spacecraft is designed to observe the Earth’s surface and to radio link the data acquired to ground complexes of data receiving, processing and dissemination for addressing a wide range of tasks to the benefit of various consumers as well as to use for developing an international cooperation of Russia in the environmental control and other actual problems relevant to the Earth remote sensing. 15
RESURS-P: General View Antenna for onboard Antenna for coordinate-time synchronizer Combined propulsion unit command&measuring system Propulsion module Solar battery Instrument module Special-purpose instrument Powered gyroscopic module complex Hyperspectral equipment Optoelectronic equipment ИУС-ВОА Sensor unit High-speed radio link antenna Star positioning unit Antenna for command Infrared sensor of local measuring system vertical Mass of fully assembled and fueled spacecraft is 5920kg Launch date – 2010 16
RESURS-P Characteristics Operational orbit - Type Near circular orbit (sun-synchronous) - Altitude, km 475 - Inclination, deg 97.3 Resolution on ground at nadir, m Н=475km - In panchromatic range 0.9 - In narrow spectral ranges 3 Swath width at nadir, km 38 (Н = 475km) Coverage area width, km 950 (Н= 475km) Spectral ranges, µm - Panchromatic 0.58÷0.8; - Narrow spectral ranges Blue (0.45÷0.52); Green (0,52 0,6); Red (0.61÷0.68; 0.72 ÷ 0.8); Red+near IR (0.8 ÷ 0.9) Spectral range number 6 Number of spectral ranges used simultaneously 1÷6 Hyperspectral imaging Available Wide-coverage multispectral imaging Available Observing interval, day 3 Maximal length of imaging, s 300 Operational data rate to receiving center, hour From RMV (РМВ) to 12 Active lifetime, years 5-7 17
Comparative Data on Swath Width of RESURS-P, RESURS-DK1 and Other Remote Sensing Spacecraft RESURS-P 38 × 38km R= 0.9m RESURS-DK1 28.3 × 28.3km R= 1m Pleiades 20 × 20 км R= 0,7м Kompsat-2 15 × 15 км R= 1м Ikonos 11 × 11 км R=1м Cartosat-2 9,6 × 9,6 км R=0,8 OrbView-3 8 × 8 км R=1м EROS-B 7 × 7 км R=0,7м 18
PROCEDURE OVERVIEW Annual Acquisition Plan Each year, before the actual start of a Quarterly Acquisition Plan Contractual Year, the FGS defines the geographical areas it One month before the Orbital Slots Request plans to image beginning of each during the coming quarter, the FGS will refine its needs for year Two weeks before a the next quarter, by Pass Programming week of acquisitions, defining the areas it the FGS expresses its intends to acquire needs in terms of Up to 36 hours before the pass, orbital slots, orbit per the FGS actually programs the orbit, day by day for instrument by providing the the whole week programming parameters described (position of the imaging segments, spectral bands selected and data rate for transmission) to the Operator. 19
TECHNOLOGIES FOR VALUE-ADDED SPACE DATA PROCESSING Value-added processing of space data enables the assessment of the Environment and natural objects conditions. · Land use monitoring (land use study; crop condition assessment; field prediction; soil mapping and soil condition assessment; agriculture control). · Forest cover and fires monitoring (forest and tundra fire seats detection; assessment of forest territories affected by fire; forest inventory; forest use study); · Water surface monitoring ( water surface temperature mapping; land surface water study; monitoring of hydro-chemical water pollution; shelf and coast marine zone study; snow and ice cover condition assessment); · Alluvial plain flooding monitoring (assessment of river plain flooding; control of water amount and estimation of flood levels; determination of flooded agricultural lands number and area; flooding damage assessment); · Ecological and geological monitoring ( ecological monitoring in the vicinity of industrial objects and large urban areas, regions of oil and gas extracting, and routes of pipelines; refinement of structural and geological maps for minerals exploration and seismic hazard assessment; observation of disaster and emergency zones). · The forecasting and space monitoring of earth- quake signs etc. 20
Monitoring spilling of oil in Kerch golf (Azov sea) 21
Monitoring spilling of oil in Kerch golf (Azov sea) 22
RESURS- DK1 Mapping USA, Albuquerque Sat. ―Resurs-DK1‖, 06.10.2007, 23
Monitoring of pipelines 24
RESURS- DK1 Urban Land Tenure Monitoring Australia, Melburn Sat. ―Resurs-DK1‖, 30.01.2006, 07:55:13 GMT 25
Mineral Industry Space Monitoring in Critical Regions Image «Resurs-DK» 26
RESURS- DK1 Environmental monitoring STEPPE FIRES MONITORING 27
RESURS- DK1 URBAN MANAGEMENT Land Tenure Monitoring France, Amien suburb Sat. ―Resurs-DK1‖, 15.10.2006, 18:07:39 GMT 28
RESURS- DK1 FORESTRY MONITORING 29
RESURS- DK1 RURAL AREAS MONITORING 30
RESURS- DK1 INDUSTRIAL AREAS MONITORING 31
Information about NTSOMZ http://eng.ntsomz.ru 32
We are open for collaboration! Address: 51, corp. 25 Dekabristov St., Moscow, 127490, Russia, NTs OMZ Phone:(495) 925-04-19, Fax: (495) 404-77-45, E-mail:ntsomz@ntsomz.ru, Internet:www.ntsomz.ru 33
Forestry Common forestland condition Unsanctioned forest slash Fire risk conditions Man's impact Forest regeneration Краснодарский край Forest mapping Республика Коми 34
AGRICULTURAL LAND MONITORING Stavropol Territory, Petrovsk Region, “Shangalinsky” SPK 35
UPDATING OF CADASTRAL PLANS Moscow region, Dolgoprudny city 36
DEFORESTATION MONITORING 37
FIRE MONITORING 38
VALUE-ADDED DATA PROCESSING NATURAL AND MAN-MADE OBJECT MONITORING Moscow region 39
ERUNET PROJECT OIL SPILL MONITORING OF THE BLACK SEA AND SEA OF AZOV 40
OSCSAR PROJECT OIL SPILL MONITORING OF THE CASPIAN SEA AND KARA SEA USING SAR 41
EARTHQUAKE FORERUNNER PREDICTION AND MONITORING 42
RESURS- DK1 IMAGE Gallery Beijing, China 43
RESURS- DK1 IMAGE Gallery Beijing, China 44
RESURS- DK1 IMAGE Gallery Shanghai, China 45
RESURS- DK1 IMAGE Gallery 46
RESURS- DK1 IMAGE Gallery 47
RESURS- DK1 IMAGE Gallery 48
RESURS- DK1 IMAGE Gallery Yanbu al Bahr, S. Arabia © NTs OMZ Abu-Dhabi, UAE © NTs OMZ ResursResurs DK image RK image 49
RESURS- DK1 IMAGE Gallery Kuwait, Kuwait © NTs OMZ Resurs DK image 50
RESURS- DK1 IMAGE Gallery Dubai,UAE © NTs OMZ Resurs DK image 51
DEVELOPMENT OF TECHNIQUES AND FACILITIES FOR SATELLITE MONITORING OF NEAR SPACE HELIGEOPHYSICAL PARAMETERS The NTs OMZ develops and exploits the onboard information and measuring instrument packages designed for the near- Earth space monitoring Mission The data obtained are transmitted on an operational basis to Heliogeophysical Service of Roshydromet to be processed and analyzed for providing authorities, population, and the Russian Federal Armed Forces with heligeophysical data including: -On-line current data and predictions on solar activity, radiation environment in the near-Earth space, the magnetosphere and ionosphere condition, and radio wave propagation conditions; -Predictions of the useable frequency bands at specified radio channels; -Urgent data on hazardous situations caused by abnormal natural heliogeophysical phenomena. Solar Constant Meter ISP-2M (ELEKTRO-L) The heliogeophysical instrument packages are used on board METEOR-3M №1 spacecraft and developed for promising METEOR-M and ELEKTRO-L. Multichannel Spectrometer for Geoactive Radiation MSGI-5EI (METEOR-3M №1) 52

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16 federal space agency of russia

  • 1. FEDERAL SPACE AGENCY OF RUSSIA RESEARCH CENTER FOR EARTH OPERATIVE MONITORING FASILITIES OF REMOUTE SENSING SPACECRAFT OPERATOR Address: 51, corp. 25 Dekabristov St., Moscow, 127490, Russia, NTs OMZ Phone:(495) 925-04-19, Fax: (495) 404-77-45, E-mail:ntsomz@ntsomz.ru, Internet:www.ntsomz.ru 1
  • 2. Operator of russian remote sensing spacecrafts The Research Center for Earth Operative Monitoring (NTs OMZ) acts as the Russian Federal Space Agency’s ground segment for space data planning, acquisition, processing, and dissemination. The NTs OMZ performs an entire technological cycle of planning, acquisition, recording, processing, archiving, storing, and dissemination of data from the ROSKOSMOS’s remote sensing spacecraft as well as from foreign satellites within the framework of concluded agreements and contracts. The NTS OMZ is equipped with the antenna systems and uses modern high technologies for space data processing and archiving, maintains a unified E-catalog and the ROSKOSMOS’s archive of the remote sensing data, provides consumers with a remote access to space data. The modern technological and methodological base allows for the foreign remote sensing spacecraft and their data to be dealt with. The NTs OMZ completing orders for operational imaging of the Earth’s surface and having a large fund of remote sensing data, offers customers remote sensing data of various spatial resolution from both the Russian and foreign satellites as well as value-added processing of the data and implementation of thematic projects. 2
  • 3. Main Tasks of Center for Operational Acquisition, Processing and Dissemination of Space Data on Earth • Acts as a parent organization of the Russian Space Agency on remote sensing space system operation to the benefit of socio-economic development of the Russian Federation and international collaboration; • Acts as an Operator for exploitation and end use of the Russian remote sensing system and provision of consumers with remote sensing data; • Provides and conducts in-flight tests of onboard scientific and information equipment; • Makes plans of imaging, provides acquisition, recording, processing, and dissemination of remotely-sensed data from the Russian spacecraft; • Provides federal, regional, departmental and commercial consumers with remote sensing data; • Creates and maintains E-catalog and fund of remote sensing data and value-added products; • Makes co-ordination and scientific and methodical supervision of the Russian and foreign centers and stations of data acquisition, processing and archiving from the Russian spacecraft; • Interacts with appropriate foreign organization on remote sensing data acquisition, processing, archiving and distributing; • Develops scientific and applied projects including international ones, to derive new data products from space observations; • Contributes to international and scientific and technical cooperation in the context of intergovernmental agreements, and performs an international exchange of space data in accordance with concluded agreements and contracts. 3
  • 4. RESURS- DK1 MISSION Multi-spectral high resolution remote sensing of the Earth’s surface designed for acquisition of high quality imagery as in near real-time as on-line to be delivered via radio link. Spacecraft and orbit parameters: Spacecraft mass - 6570 kg Payload mass - 1200 kg Altitude - H=360-604 km Inclination - 70,0° RESURS- DK1 Modules and Blocks 4
  • 5. RESURS- DK1 SPECIFICATIONS Remote-sensing instrument features: • Multispectral capabilities - 3 spectral bands. • Spectral bands: • 1-3 spectral bands to be recorded simultaneously; • wavelengths are 0,58-0,8 micrometers (panchromatic mode), 0,5-0,6, 0,6-0,7, 0,7-0,8 (narrow bands in multispectral mode). • Spatial resolution – 1,0m in panchromatic mode and 2,0-3,0 m in narrow bands at nadir, 350 km altitude, 30º sun elevation angle over local horizon. • Swath width at the altitude of 350 km at nadir is 28,3 km, 57km at ±45º incidence angle (roll). • Field of view at the altitude of 350 km is 700 km (±45º inclination). • Position accuracy by orbital data is 100 m. • Revisiting frequency at nadir is 3-6 days. • Observation time for stripes - from 2 to 300 s. • Maximum technical capacity – 1 mln. sq. km per day. 5
  • 7. RESURS- DK1 Applications • Data supply for resource management and economical activity (inventory of natural resources, topographic and thematic mapping); • Monitoring of pollution sources of the atmosphere, water and soil with the view of providing Federal and regional environmental authorities with the relevant information to make management decisions; • On-line monitoring of man-caused and natural emergencies for the purpose of effective planning and timely performing of measures to eliminate damages; • Supplying home and foreign consumers on a commercial basis; • Research activities (PAMELA Experiment — space exploration to search and study antimatters: antiprotons, positrons, nuclear and electronic components in primary space radiation). 7
  • 8. Comparative Data over Areas Imaged from Multiple Remote Sensing Spacecraft OrbView - 3 8 x 8 km 8 x 8 км Lм=0,6 м IKONOS 11 x 11 km 11 x 11км Lм=1 м SPOT 60 x 60 km 60 x 60км Lм=2,5 м RESURS RESURS - DK1 28 x 28 km 28 x 28км Lм=1 м 8
  • 9. KANOPUS-V Space System Designed for Operational Monitoring of Anthropogenic and Natural Emergencies Mission Purpose Panchromatic and multi-spectral imaging of the Earth Recording of abnormal physical phenomena for earthquake prediction Spacecraft mass - 350kg Payload mass - 147kg Altitude - H=510-600km Inclination (ССО) - 98° Lifetime – 7 years Launch date - 4th quarter of 2009 KANOPUS-V Modules and Blocks 9
  • 10. KANOPUS-V Main Characteristics : • Multi-spectral capabilities - 4 spectral bands; • Spectral bands: • 1-4 spectral bands designed for simultaneous recording; • Wavelength 0.52-0.85 µm (panchromatic mode), 0.54-0.6, 0.63-0.69, 0.69-0.72, 0.75-0.86 µm (narrow ranges in multi-spectral mode); • Spatial resolution – 2.7m in panchromatic mode and 12.0m in narrow ranges at nadir from 510-km altitude; • Field of view at altitude of 510km at nadir – more than 20.0km; • Swath width at altitude of 510km - 1020km (angle of roll ±45º); • Image repeat possibility at nadir (at the equator) – 5 days; • Observing time along the route – up to 350s; • Maximal performance – 500 000 sq. km per day. 10
  • 11. KANOPUS-V Main Applications • Monitoring of man-made and natural emergencies including natural hydrometeorological disasters; • Detection of forest fire seats, large pollutant emissions; •Monitoring of agricultural activity, natural resources (including water and coastal resources); • Land use; • Operational observation of specified areas of the earth’s surface; • Recording of abnormal physical phenomena in the atmosphere, ionosphere, magnetosphere, and at the Earth’s surface in an effort to predict earthquakes. 11
  • 12. METEOR-M №1 Spacecraft SEVERYANIN-M On-board Radar Complex (BRLK) Module for Atmospheric Temperature and Humidity Sounding (MTVZA) Meteorological Multi-Band Scanning Device (MSU-MR) Decimetric Radio Link Centimetric Radio Link Multi-Band Imagery Complex Data Collection and for Ecological Heliogeophysical Equipment Transmission System monitoring (KMSS) (GGAK) (SSPD) 12
  • 13. METEOR-M SPACE SYSTEM Mission Purpose - Acquisition of multiband images Spacecraft mass - 3000kg including radar ones and Orbital altitude - H=830.00km measurements of the ―Earth’s surface – Atmosphere‖ system Inclination (ССО) - 98.85° outgoing radiation over various Orbital period - 101.3min regions of the energy spectrum in terms of absolute radiant qualities; Lifetime - 5 years - Heliogeophysical data acquisition; - Collection and transmission of data Launch date - 2nd quarter of 2009 from automatic data collection platforms (DCP) of different types (ground-based, ice, drifting) deployed in any region of the Earth (including the polar regions). 13
  • 14. METEOR-M Spacecraft Main Characteristics : MSU-MR: KMSS: - Swath width – 2800km; - Swath width when two cameras operate - Spatial resolution on ground -1000m; simultaneously - 1000-1200km; - Spectral band number – 6; - Resolution – 70m; - Rated values of spectral bands - 0.5-0.7; 0.7-1,1; -Spectral band number - 4; 1.6-1.8; - Rated values of spectral bands - 0.45-0.50; 3.5-4.1; 10.5-11.5; 11.5-12.5µm; 0.535-0.575; 0.63-0.68; 0.76-0,9 µm. - Range of radiation temperatures measured 213-313 °К. MTVZA: BRLK: - Swath width – 1500km; - Swath width – 600km; - Channel number - 26; - Linear resolution on ground - Spatial resolution - 16 – 198km; - 400 – 650m (moderate resolution mode) - Vertical resolution - 4 – 5km; - 800 – 1300m (low resolution mode); - Operating frequency range – 18.7 – 183.31 - Wavelength of sounding pulse - 3.12cm . GHz. 14
  • 15. RESURS-P: Mission Purpose The RESURS-P spacecraft is designed to observe the Earth’s surface and to radio link the data acquired to ground complexes of data receiving, processing and dissemination for addressing a wide range of tasks to the benefit of various consumers as well as to use for developing an international cooperation of Russia in the environmental control and other actual problems relevant to the Earth remote sensing. 15
  • 16. RESURS-P: General View Antenna for onboard Antenna for coordinate-time synchronizer Combined propulsion unit command&measuring system Propulsion module Solar battery Instrument module Special-purpose instrument Powered gyroscopic module complex Hyperspectral equipment Optoelectronic equipment ИУС-ВОА Sensor unit High-speed radio link antenna Star positioning unit Antenna for command Infrared sensor of local measuring system vertical Mass of fully assembled and fueled spacecraft is 5920kg Launch date – 2010 16
  • 17. RESURS-P Characteristics Operational orbit - Type Near circular orbit (sun-synchronous) - Altitude, km 475 - Inclination, deg 97.3 Resolution on ground at nadir, m Н=475km - In panchromatic range 0.9 - In narrow spectral ranges 3 Swath width at nadir, km 38 (Н = 475km) Coverage area width, km 950 (Н= 475km) Spectral ranges, µm - Panchromatic 0.58÷0.8; - Narrow spectral ranges Blue (0.45÷0.52); Green (0,52 0,6); Red (0.61÷0.68; 0.72 ÷ 0.8); Red+near IR (0.8 ÷ 0.9) Spectral range number 6 Number of spectral ranges used simultaneously 1÷6 Hyperspectral imaging Available Wide-coverage multispectral imaging Available Observing interval, day 3 Maximal length of imaging, s 300 Operational data rate to receiving center, hour From RMV (РМВ) to 12 Active lifetime, years 5-7 17
  • 18. Comparative Data on Swath Width of RESURS-P, RESURS-DK1 and Other Remote Sensing Spacecraft RESURS-P 38 × 38km R= 0.9m RESURS-DK1 28.3 × 28.3km R= 1m Pleiades 20 × 20 км R= 0,7м Kompsat-2 15 × 15 км R= 1м Ikonos 11 × 11 км R=1м Cartosat-2 9,6 × 9,6 км R=0,8 OrbView-3 8 × 8 км R=1м EROS-B 7 × 7 км R=0,7м 18
  • 19. PROCEDURE OVERVIEW Annual Acquisition Plan Each year, before the actual start of a Quarterly Acquisition Plan Contractual Year, the FGS defines the geographical areas it One month before the Orbital Slots Request plans to image beginning of each during the coming quarter, the FGS will refine its needs for year Two weeks before a the next quarter, by Pass Programming week of acquisitions, defining the areas it the FGS expresses its intends to acquire needs in terms of Up to 36 hours before the pass, orbital slots, orbit per the FGS actually programs the orbit, day by day for instrument by providing the the whole week programming parameters described (position of the imaging segments, spectral bands selected and data rate for transmission) to the Operator. 19
  • 20. TECHNOLOGIES FOR VALUE-ADDED SPACE DATA PROCESSING Value-added processing of space data enables the assessment of the Environment and natural objects conditions. · Land use monitoring (land use study; crop condition assessment; field prediction; soil mapping and soil condition assessment; agriculture control). · Forest cover and fires monitoring (forest and tundra fire seats detection; assessment of forest territories affected by fire; forest inventory; forest use study); · Water surface monitoring ( water surface temperature mapping; land surface water study; monitoring of hydro-chemical water pollution; shelf and coast marine zone study; snow and ice cover condition assessment); · Alluvial plain flooding monitoring (assessment of river plain flooding; control of water amount and estimation of flood levels; determination of flooded agricultural lands number and area; flooding damage assessment); · Ecological and geological monitoring ( ecological monitoring in the vicinity of industrial objects and large urban areas, regions of oil and gas extracting, and routes of pipelines; refinement of structural and geological maps for minerals exploration and seismic hazard assessment; observation of disaster and emergency zones). · The forecasting and space monitoring of earth- quake signs etc. 20
  • 21. Monitoring spilling of oil in Kerch golf (Azov sea) 21
  • 22. Monitoring spilling of oil in Kerch golf (Azov sea) 22
  • 23. RESURS- DK1 Mapping USA, Albuquerque Sat. ―Resurs-DK1‖, 06.10.2007, 23
  • 25. RESURS- DK1 Urban Land Tenure Monitoring Australia, Melburn Sat. ―Resurs-DK1‖, 30.01.2006, 07:55:13 GMT 25
  • 26. Mineral Industry Space Monitoring in Critical Regions Image «Resurs-DK» 26
  • 28. RESURS- DK1 URBAN MANAGEMENT Land Tenure Monitoring France, Amien suburb Sat. ―Resurs-DK1‖, 15.10.2006, 18:07:39 GMT 28
  • 30. RESURS- DK1 RURAL AREAS MONITORING 30
  • 32. Information about NTSOMZ http://eng.ntsomz.ru 32
  • 33. We are open for collaboration! Address: 51, corp. 25 Dekabristov St., Moscow, 127490, Russia, NTs OMZ Phone:(495) 925-04-19, Fax: (495) 404-77-45, E-mail:ntsomz@ntsomz.ru, Internet:www.ntsomz.ru 33
  • 34. Forestry Common forestland condition Unsanctioned forest slash Fire risk conditions Man's impact Forest regeneration Краснодарский край Forest mapping Республика Коми 34
  • 35. AGRICULTURAL LAND MONITORING Stavropol Territory, Petrovsk Region, “Shangalinsky” SPK 35
  • 36. UPDATING OF CADASTRAL PLANS Moscow region, Dolgoprudny city 36
  • 39. VALUE-ADDED DATA PROCESSING NATURAL AND MAN-MADE OBJECT MONITORING Moscow region 39
  • 40. ERUNET PROJECT OIL SPILL MONITORING OF THE BLACK SEA AND SEA OF AZOV 40
  • 41. OSCSAR PROJECT OIL SPILL MONITORING OF THE CASPIAN SEA AND KARA SEA USING SAR 41
  • 43. RESURS- DK1 IMAGE Gallery Beijing, China 43
  • 44. RESURS- DK1 IMAGE Gallery Beijing, China 44
  • 45. RESURS- DK1 IMAGE Gallery Shanghai, China 45
  • 46. RESURS- DK1 IMAGE Gallery 46
  • 47. RESURS- DK1 IMAGE Gallery 47
  • 48. RESURS- DK1 IMAGE Gallery 48
  • 49. RESURS- DK1 IMAGE Gallery Yanbu al Bahr, S. Arabia © NTs OMZ Abu-Dhabi, UAE © NTs OMZ ResursResurs DK image RK image 49
  • 50. RESURS- DK1 IMAGE Gallery Kuwait, Kuwait © NTs OMZ Resurs DK image 50
  • 51. RESURS- DK1 IMAGE Gallery Dubai,UAE © NTs OMZ Resurs DK image 51
  • 52. DEVELOPMENT OF TECHNIQUES AND FACILITIES FOR SATELLITE MONITORING OF NEAR SPACE HELIGEOPHYSICAL PARAMETERS The NTs OMZ develops and exploits the onboard information and measuring instrument packages designed for the near- Earth space monitoring Mission The data obtained are transmitted on an operational basis to Heliogeophysical Service of Roshydromet to be processed and analyzed for providing authorities, population, and the Russian Federal Armed Forces with heligeophysical data including: -On-line current data and predictions on solar activity, radiation environment in the near-Earth space, the magnetosphere and ionosphere condition, and radio wave propagation conditions; -Predictions of the useable frequency bands at specified radio channels; -Urgent data on hazardous situations caused by abnormal natural heliogeophysical phenomena. Solar Constant Meter ISP-2M (ELEKTRO-L) The heliogeophysical instrument packages are used on board METEOR-3M №1 spacecraft and developed for promising METEOR-M and ELEKTRO-L. Multichannel Spectrometer for Geoactive Radiation MSGI-5EI (METEOR-3M №1) 52