[2024]Digital Global Overview Report 2024 Meltwater.pdf
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
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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.
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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.
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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).
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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
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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
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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.
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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.
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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)
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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).
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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.
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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.
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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
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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
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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
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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.
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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.
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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
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34. Forestry
Common forestland
condition
Unsanctioned forest
slash
Fire risk conditions
Man's impact
Forest regeneration Краснодарский край
Forest mapping
Республика Коми
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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)
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