Robust Imaging from Space

Adjunct Reference Document #1

Satellite and Airborne SAR Sensor Specifications

The following tables provide detailed specifications of currently operational and proposed satellite and airborne SAR sensors, including those having reached end of life.

Table A - Operational satellite SAR sensors and specifications ______1 Table B - Future/proposed satellite SAR sensors and specifications. ______7 Table C - Operational airborne SAR sensors and specifications. ______13 Table D - Decommissioned SAR sensors. ______18

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table A - Operational satellite SAR sensors and specifications

Table A - Operational satellite SAR sensors and specifications X-BAND

Sensor, operating agency, launch, Design life (EOL), Orbit & altitude (km) Swath Imaging modes Spatial Incidence application area Inclination angle (°) width resolution angle (°)

Target revisit time (km) (m) Nation

SAR-Lupe 1-5 Polar X-band SAR DLR/Bundeswehr 500 km Encrypted S-band for telemetry & command  5 for delivering high resolution 98.2° transmissions SAR images for military reconnaissance Daily 8 Stripmap mode 1st 2006, 2nd 2007, 3rd 2007, 4th 2008, 5th 2008 5.5 Spotlight mode <1 Est. Cost 250 mil EUR EOL: 10 yrs

TSX-1 (TerraSAR-X) Sun-synch X- Multiple imaging modes DLR, 2007-2013 514 km 10 High resolution Spotlight SP (HH or VV) or 1.48-3.49 20-55  Scientific & commercial use hydrology, geology, 97.44° DP (HH/VV) climatology, oceanography, environment & disaster 11 days 10 Spotlight SP (HH or VV) or DP (HH/VV) 1.48-3.49 20-55 monitoring, cartography Stripmap SP (HH or VV) or DP (HH/VV, 15-30 HH/HV, VV/VH) 1.7-3.49 20-45 ScanSAR SP

GERMANY 100 1.7-3.49 20-45 Left and right looking TDX-1 (TanDEM-X) Sun-synch Interferometric imaging: 12 (DEM) 25-55 DLR, 2010-2014 514 km Bistatic mode (abs v.acc 10  Global DEM generation & earth observation, new 97.44° Monostatic mode m, rel acc. applications using along-track InSAR (e.g., measuring 11 days Along-track interferometry (ATI) <2 m) ocean currents), pol-InSAR, bistatic processing and Polarimetric interferometry formation flying SAR imaging (same as TerraSAR-X): EOL: 5 yrs 30 Stripmap DP 3 Co-fly in close formation with TSX-1, near identical 10 Spotlight DP 1 capability 100 ScanSAR DP 16

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table A - Operational satellite SAR sensors and specifications

X-BAND

Sensor, operating agency, launch, Design life (EOL), Orbit & altitude (km) Swath Imaging modes Spatial Incidence application area Inclination angle (°) width resolution angle (°)

Nation Target revisit time (km) (m)

Cosmo-SkyMed 1-4 (Constellation of small Satellites Sun-synch Selectable single pol (HH,VV,HV,VH) 25-50 for Mediterranean basin Observation) 620 km Spotlight Left and ITA, -1 2007, -2 2007, -3 2008, -4 2009 97.86° 10 Stripmap 1 right looking EOL: 5 years Daily-16 days 30-40 ScanSAR 3-15 4 X-band EOS satellite constellation 100-200 Ping pong or Stripmap – 2x selectable pol 30-100 Dual use: 30 (HH, VV, HV, VH) 15

ITALY  Civilian: disaster/risk management, ice monitoring, agriculture, urban  Defence: intelligence gathering, ship detection, maritime surveillance, security

Meteor-M N1 (Meteorological Satellite) Sun-synch 450-600 Onboard Radar Complex (OBRC) – 400-1000 25-48 ROSHYDROMET, ROSKOSMOS. 2009-2014 830 km Severjanin, Vertical pol EOL: 5 yrs 98.79° Low resolution MSS (MSU-MR)  Operational meteorological services, regional & 37 days IR Fourier Spectrometer (IRFS-2) global weather analysis & prediction, ocean surface MS imaging system (KMSS) water states, space weather analysis Microwave imaging/sounding radiometer RUSSIA (MTVZA) Spectrometer for Geoactive Measurements (MSGI) Data Collection System (DCS) IGS-7A Polar 1 (Information Gathering Satellite) 500 km

2011- Dual use  Military: surveillance, early warning of hostile JAPAN launches  Civilian: disaster monitoring

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table A - Operational satellite SAR sensors and specifications

X-BAND

Sensor, operating agency, launch, Design life (EOL), Orbit & altitude (km) Swath Imaging modes Spatial Incidence application area Inclination angle (°) width resolution angle (°)

Nation Target revisit time (km) (m)

RISAT-2 (Radar Imaging Satellite 2) Sun-synch 10-50 Spotlight 3-8 ISRO, 2009-2013 550 km Stripmap Dual use Mosaic mode  Civil: agriculture, forestry, soil moisture, geology, sea ice, coastal processes, object detection, flood

INDIA mapping  Military: reconnaissance, border surveillance, ship detection

TecSAR (Technological SAR) 450-580 km Selectable pol (HH,HV,VH,VV)

IAI, 2008- 41° Stripmap 1 EOL: 4 yrs Spotlight  Low-earth orbit reconnaissance ScanSAR ISRAEL Mosaic mode

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table A - Operational satellite SAR sensors and specifications

C-BAND

Sensor, operating agency, launch, Design life (EOL), Orbit & altitude (km) Swath Imaging modes Spatial Incidence application area Inclination angle (°) width resolution angle (°)

Nation Target revisit time (km) (m)

RISAT-1 (Radar Imaging Satellite) Sun-synch circ 10 Spotlight SP/DP <2 ±34 ISRO, 2012-2017 609 km 30 Stripmap mode-1 (FRS-1) SP/DP 3 Left or right EOL: 5 yrs 97.84° 30 Stripmap mode-2 (FRS-2) QP 12 looking Dual use 12 days 120 Med res ScanSAR (MRS) SP/DP 25  Civil: agriculture, forestry, soil moisture, geology, 240 Coarse res ScanSAR (CRS) SP/DP 50

INDIA sea ice, coastal processes, object detection, flood mapping  Military: reconnaissance, border surveillance, ship detection -1 Sun-synch C- Multiple imaging modes CSA, 1995- 798 km 45 Fine HH 8 37-47  Earth observation: disaster management, 98.6° 100 Standard HH 30 20-49 interferometry, agriculture, cartography, hydrology, 24 days 150 Wide HH 30 20-45 forestry, oceanography, ice studies, coastal 300 ScanSAR narrow 50 20-49 monitoring 500 ScanSAR wide 100 29-49 75 Extended high 18-28 52-58 170 Extended low 30 10-22

Right looking

RADARSAT-2 Sun-synch Multiple imaging modes CSA, 2007- 798 km 20 Ultra-Fine SP 3 30-49  Earth observation: maritime surveillance, disaster 98.6° 50 Multi-look Fine SP 8 30-50

CANADA management, ecosystem monitoring 24 days 50 Fine SP/DP 8 30-50 100 Standard SP/DP 25 20-49 150 Wide SP/DP 30 20-45 300 ScanSAR Narrow SP/DP 50 20-46 500 ScanSAR Wide SP/DP 100 20-49 75 Extended High SP 18 49-60 25 Fine QP 12 20-41 25 Standard QP 25 20-41

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table A - Operational satellite SAR sensors and specifications

S-BAND

Sensor, operating agency, launch, Design life (EOL), Orbit & altitude (km) Swath Imaging modes Spatial Incidence application area Inclination angle (°) width resolution angle (°)

Nation Target revisit time (km) (m)

Kondor-E Polar 20-150 Spotlight HH, VV 1-2 20-55 NPO, 2012-2022 800 km 10-20 Stripmap 1-3 Left and EOL: 3-10 yrs ScanSAR 5-30 Right looking

Dual use  Military: navigation and reconnaissance  Earth observation: agriculture, forestry, land use

RUSSIA management, geology and mineral exploration,  environmental protection

HJ-1C (Huan Jing-1) Sun-synch circ 1 radar + 2 optical constellation (HJ-1A: 31-44.5 CRESDA, 2011-2014 500 km CCD+IR camera, HJ-1B: CCD+HSI camera)  Environmental monitoring & prediction, solid waste 97.3° StripMap SP (HH or VV) monitoring, disaster monitoring & prediction (flood, 31 days ScanSAR drought, typhoon, wind damage, sand storm, 40 5 earthquake, land creep, frost, grassland fires, crop 100 20

CHINA pests, ocean disaster monitoring)

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table A - Operational satellite SAR sensors and specifications

L-BAND

Sensor, operating agency, launch, Design life (EOL), Orbit & altitude (km) Swath Imaging modes Spatial Incidence application area Inclination angle (°) width resolution angle (°)

Nation Target revisit time (km) (m)

JianBing-5 (JB-5) 635 km (Y3) 20 Spotlight 5 63.4 (Y9) JB 5-2/Yaogan3, JB 9-1/Yaogan6, JB 9-2/Yaogan8, 518 km (Y6) 100 ScanSAR 40 Yaogan9A/9B/9C, JB 9-3/Yaogan10, Yaogan13 1200 km (Y8) 1.5 (Y6)

Y3 2007-, Y6 2009-, Y8 2009-, Y9 2010-, Y10 2010-, Y13 1089 km (Y9) 2011 629 km (Y10) Dual use 97.8 ° CHINA  Military: intelligence gathering, surveillance and reconnaissance  Earth observation: land survey, disaster forecasting, crop yield evaluation, urban planning

MULTI-FREQUENCY

Sensor, operating agency, launch, Design life (EOL), Orbit & altitude (km) Swath Imaging modes Spatial Incidence application area Inclination angle (°) width resolution angle (°)

Nation Target revisit time (km) (m) Smotr Gascom, 2009 Sun-synch X- or C-band EOL: 7-10 yrs 670 km 10-15 High resolution mode 1-3  4 low-orbit satellites for monitoring oil/gas pipeline 98° 30-100 Low resolution mode 5-15 and earth observation (2 radar, 2 optical)

Priroda 400 km 50 Radiometer, SAR and optical imaging 50 35 RUSSIA RKA, 1996- 52° L-HH and S-VV  Launched & installed on MIR space station 6 days  Geoecology, land surface & ocean exploration

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table B - Future/proposed satellite SAR sensors and specifications

Table B - Future/proposed satellite SAR sensors and specifications

X-BAND

Sensor, operating agency, launch, design life (EOL), Orbit & altitude (km) Swath Imaging modes Spatial Incidence application area Inclination angle (°) width resolution angle (°)

Nation Target revisit time (km) (m) SEOSAR/ (SAR Observation Spanish Satellite) Sun-synch Based on TerraSAR-X 15-60 2012-2016 514 km 5-10 Spotlight SP/DP 1-2 Left and

Dual use 97.44° 15-30 Stripmap SP/DP 3-6 right looking  Defence: land/water surveillance, border control, 11 days 100 ScanSAR (HH, VV) 15 tactical support SPAIN  Civil: natural disaster monitoring, risk & crisis management

Cosmo-SkyMed Second Generation (CSG-1, CSG-2) Sun-synch 10 Spotlight DP 1 ASI, MiD 620 km 40 Stripmap DP 3 CSG-1 2015-2023, CSG-2 2016-2023 97.8° 100, 200 ScanSAR DP 20, 40  Environmental monitoring, surveillance and risk 16 days 30 Ping-pong QP 15

ITALY management, maritime, topographic mapping, law enforcement

TerraSAR-X2 Sun-synch Spotlight 0.5 DLR, 2015-2018 10-40 Stripmap 1-4  Commercial follow-on mission to TSX-1: 50-500 ScanSAR 5-50 cartography, land surface, civil planning, DTMs,

GERMANY environmental monitoring AstroSAR Sun-synch 10 Spotlight SP (HH or VV) or DP (HV) 1 ±45 Astrium 500 km Stripmap SP/DP Left and EOL: 5 yrs 20 ScanSAR SP/DP 3 right looking Mini-satellite proposed to UK Ministry of Defence Hourly-daily 100 Maritime 30

UK Cost: <$100 mil. 900 20 Dual use:  civil/military Maritime, environment, security & disaster monitoring

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table B - Future/proposed satellite SAR sensors and specifications

X-BAND

Sensor, operating agency, launch, design life (EOL), Orbit & altitude (km) Swath Imaging modes Spatial Incidence application area Inclination angle (°) width resolution angle (°)

Nation Target revisit time (km) (m) -M N2, N3 (Meteorological Satellite) Sun-synch 450-600 Onboard Radar Complex (OBRC) – 400-1000 25-48 ROSHYDROMET, ROSKOSMOS, N2 2012, N3 2015 835 km Severjanin, Vertical pol EOL: 5 yrs 98.7° Module for Geophysical Measurements

 Operational meteorological services, regional & 37 days (GGAK-M)

global weather analysis & prediction, ocean surface Fourier spectrometer (IKFS-2) water states, space weather analysis MS imager (KMSS)

MS scanning imager/radiometer (MSU-MR) RUSSIA Scanning microwave imager-sounder (MTVZA) Data Collection System (DCS)

KOMPSAT-5 (Korea Multi-Purpose Satellite-5) Sun-synch Selectable pol (HH,HV,VH,VV) 20-55

KARI, 2012-2017 550 km High resolution mode EOL; 5 yrs 97.6° 5 Standard mode 1  Civil/scientific use; GIS, ocean & land management, 28 days 30 Wide swath mode 3 KOREA environment and disaster monitoring 100 20

RISAT-2F (Radar Imaging Satellite) Sun-synch

ISRO, 2013-? 550 km  Research and disaster management applications

INDIA

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table B - Future/proposed satellite SAR sensors and specifications

C-BAND

Sensor, operating agency, launch, design life (EOL), Orbit & altitude (km) Swath Imaging modes Spatial Incidence application area Inclination angle (°) width resolution angle (°)

Target revisit time (km) (m) Nation

Sentinel-1 A,B,C 693 km VV+VH, HH+HV 20-45

ESA 98.18° 80 StripMap 5 A 2012-2020, B 2014-2022, C 2019-2026 12 days 250 Interferometric Wide swath 5x20

 Sea ice monitoring, marine surveillance, land surface Extra wide swath ITALY motion, disaster management 400 Wave mode 20x40 5x5 RADARSAT Constellation Mission (RCM) C-1, C-2, C-3 592.7 km HH,VV,HV,VH, compact pol CSA, C1,C2 2014-2021, C3 2015-2022 97.74° Low resolution  3 EOS satellites for near real-time maritime 12 days 500 Med resolution (maritime) 100 19-54

surveillance (ship detection, oil spill monitoring & 350 Med resolution (land) 50 19-58 sea ice mapping), disaster management, InSAR for 30 Med resolution (land) 16 20-47 geohazards, climate change & environment 125 High resolution 30 21-47 monitoring 30 Very high resolution 5 19-54 20 Ice/oil low noise 3 18-54 350 25 m ship mode 100 19-58 350 variable 19-58 Right looking

S-BAND

Sensor, operating agency, launch, design life (EOL), Orbit & altitude (km) Swath Imaging modes Spatial Incidence application area Inclination angle (°) width resolution angle (°)

Nation Target revisit time (km) (m) NovaSAR-S Sun-synch or LI SP/DP/TP: (HH, HV, VH, VV) SSTL, 2013-2020 equatorial 15-20 Stripmap 6 16-34  Scientific/EO: flood and disaster monitoring, 580 km 100 ScanSAR 20 16-30

UK forestry, maritime surveillance, agriculture, land Daily-4 days 150 ScanSAR wide 30 15-31 cover/use 750 Maritime surveillance 30 48-73

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table B - Future/proposed satellite SAR sensors and specifications

L-BAND

Sensor, operating agency, launch, design life (EOL), Orbit & altitude (km) Swath Imaging modes Spatial Incidence application area Inclination angle (°) width resolution angle (°)

Target revisit time (km) (m) Nation

TanDEM-L 760 km 350 L-band SAR 20-100 26.3-46.6 DLR, 2017-2022 Single-pass InSAR 8 days Polarimetry - quad

Wide swath mode GERMANY

ALOS PALSAR-2 628 km 25 Spotlight SP 3x1 30-44 (Phase Array L-band SAR) 97.9° 50 Ultra Fine SP/DP 3 Left or right

JAXA, 2013-2017 14 days 50 High sensitive SP/DP/FP/CP 6 looking

 Earth observation, interferometry 66 days 70 Fine SP/DP/FP/CP 10 42 days 350 ScanSAR nominal SP/DP 100

JAPAN 14 days 490 ScanSAR wide SP/DP 60 (*SP: HH or VV or HV; DP: HH+HV or VV+VH; FP: HH+HV+VH+VV; CP: compact pol)

RISAT-1F and -3L (Radar Imaging Satellite) Sun-synch SAR L-radiometer ISRO, 1F 2012-2018, 3L 2014-2020 Dual use 97.84°  Civil: agriculture, forestry, soil moisture, geology, 12 days sea ice, coastal processes, object detection, flood

INDIA mapping  Military: reconnaissance, border surveillance, ship detection

DESDNyl Sun-synch 180-240 Multiple polarisations 10-100

NASA JPL, 2017-2022 600-800 km Single/dual-pol repeat pass InSAR

 Earth observation: land surface change & hazards, 97° Expt. quad-pol repeat pass InSAR USA terrestrial & climate variables 12-16 days

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table B - Future/proposed satellite SAR sensors and specifications

L-BAND

Sensor, operating agency, launch, design life (EOL), Orbit & altitude (km) Swath Imaging modes Spatial Incidence application area Inclination angle (°) width resolution angle (°)

Target revisit time (km) (m) Nation

SMAP (Soil Moisture Active Passive) Sun-synch 1000 L-band SAR VV,HH,HV 1-3 km 40 NASA JPL, 2014-2017 680 km L-band Radiometer 40 km  Global measurements of soil moisture and freeze/thaw state for improved understanding of 2-3 days water, energy & carbon cycles, climate modelling, flood prediction, drought monitoring

SAOCOM (SAR Observation and Communications Sun-synch 20-40 Stripmap SP/DP 10 17-50.4

Satellite) 620 km 100-150 TopSAR narrow SP/DP/QP 30-50 17.6-47.3 CONAE, Argentina and ASI, Italy 97.89° 220-350 TopSAR wide SP/DP/QP/CL 50-100 17.6-48.9 Satellite EOS constellation 16 days (1 sat) (*SP: HH or HV or VH or VV; DP: HH+HV or Right looking 1A 2014-2019, 1B 2015-2020, 2A 2015-2020, 2B 2016- 8 days (const) VV+VH; QP: HH+HV+VH+VV; CL: RH+RV or 2021 LH+LV) EOL: 5 yrs  Soil moisture mapping to support agricultural, hydrological & health applications, General NRM &

disaster management ARGENTINA & ITALY ARGENTINA &

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table B - Future/proposed satellite SAR sensors and specifications

P-BAND Sensor, operating agency, launch, design life (EOL), Orbit & altitude (km) Swath Imaging modes Spatial Incidence application area Inclination angle (°) width resolution angle (°)

Nation Target revisit time (km) (m) BIOMASS 642 km P-band InSAR full pol 50x65 23-32 ESA, Italy, 2016-2021 60 StripMap Left or right 25-45 days 105 ScanSAR looking ITALY

MULTI-FREQUENCY

Arkon-2M Sun-synch 550-600 2-10 X- 1-1.5

Roskosmos, 2013-2018 km 20-100 L- 3-5  Military surveillance, earth observation and weather 100-450 R- (69 cm) 30

information RUSSIA

HY-3A, HY-3B, HY-3C Sun-synch 20-40 X- SAR Precise mode HH,VV 1 15-60 CRESDA 799 km 60-80 X- Stripmap HH,VV 5 3A 2015-2020, 3B 2017-2022, 3C 2022-2027 98.48° 120-150 X- ScanSAR HH,VV 10

EOL: >3 yrs 29 days 5 C- SAR Wave mode HH+VV or HH+HV or 10

 Ocean monitoring, environmental protection, VV+VH coastal zone survey 150 C- Image mode HH+VV or HH+HV or VV+VH 25

CHINA 650 C- Wide swath mode HH+VV or HH+HV or 100 VV+VH 650 C- Global monitoring mode HH+VV or 1000 HH+HV or VV+VH

SCLP (Snow and Cold Land Processes) Sun-synch K-band radiometer 50-100 NASA JPL, 2030-2033 Ku and X-band radars

USA  Snow accumulation for freshwater availability 15 days

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table C - Operational airborne SAR sensors and specifications

Table C - Operational airborne SAR sensors and specifications

Sensor, operating agency and date, application area Flying height (km) Swath Frequency Spatial Incidence width Imaging modes resolution angle (°)

Nation (km) (m)

EUROPE Sethi Multispectral & SAR system ONERA, 2007- X-

 Earth observation, interferometry, security and L-, P- 0-90

scientific applications (e.g., Tropisar campaign – 5-165 preparation for BIOMASS satellite mission) RAMSES P-, L-, S-, C-, X- full pol 40-80 FRANCE ONERA Ku, Ka full pol  Scientific: topography, subsidence, vegetation, W geology, soil moisture DO-SAR S-VV, VH, HH, HV Dornier C-VV, VH, HH, HV X-VV, VH, HH, HV Ka-VV E-SAR 3.9 L- full pol 2x0.085 20-60 DLR, 1989/94- X-VV or HH GERMANY X-VV or HH P- full pol

DRA-SAR (Defence Research Agency SAR) C- full pol

UK DRA X-HH

EMISAR C- full pol 2

EMI/TUD, 1993/94- L- full pol DENMARK

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table C - Operational airborne SAR sensors and specifications

Sensor, operating agency and date, application area Flying height (km) Swath Frequency Spatial Incidence width Imaging modes resolution angle (°)

Nation (km) (m)

CARABAS (Coherent All Radio Band Sensing) 1-5 1-5 VHF 20-90 MHz 3 40-70 FOA HH  Wide-area surveillance, target detection, vegetation

and biomass, disaster monitoring SWEDEN

PHARUS (Phased Array Universal SAR) 6-20 C- full pol 3 10-75 FEL-TNO, Delft, 1995-  Military (target detection, cartography) and civil use

(forestry, agriculture, oceans) NETHERLANDS RUSSIA SAR TRAVERS S- VV or HH Vega, Moscow

IMARC 24 X-, L-, P- full polarimetric 4-15 Vega, Moscow VHF (118 MHz)

 Soil & terrain mapping, hydrology studies, DEM generation

ASIA Pi-SAR-L (Polarimetric and Interferometric SAR) 6-12 15 X- InSAR 3x3.2 10-60 JAXA, 1996- Mode 1 HH or VV  Disaster monitoring & earth observation X- and L- full pol

Mode 2 HH, HV, VH, HH NASAR-1 20 L- full pol 3

NASDA/EORC, 1996- JAPAN

NECSAR X-HH NASDA/EORC, 1992-  Interferometry & topographic mapping

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table C - Operational airborne SAR sensors and specifications

Sensor, operating agency and date, application area Flying height (km) Swath Frequency Spatial Incidence width Imaging modes resolution angle (°)

Nation (km) (m)

CASSAR 7.2 X-HH, VV 10 73-83 CAS/ISRA  Agriculture, soil moisture, vegetation parameters,

CHINA biomass, surface roughness

AUSTRALIA INGARA X- full pol 45-89 DSTO 12-48 Stripmap 2-8  Scientific: coherent change detection studies & Spotlight 0.3 feature extraction Interferometric PLIS (Polarimetric L-band Imaging SAR) 0.3-3 0.1-2.2 L-band scatterometer 11-29 15-45 Flinders University, Adelaide Full pol Left and  Test bed for SMAP with applications in soil moisture Single pass InSAR right looking estimation

SOUTH AFRICA SASAR-1 (South African SAR) 4 VHF (0.141 GHz) full pol University of Cape Town, 1999-  Terrain mapping, vegetation studies CANADA STAR-1,2 (Sea ice and Terrain Assessment Radar) 19-50 X-HH 5-18 Intermap, 1990-  Sea ice monitoring, terrain analysis

NORTH AMERICA GeoSAR 10-12 10-12 X- and P- 1.25-3 (X-) 25-60 Interferometer and LiDAR profiler HH+HV or VV+VH 1.25-5 (P-) Fugro EarthData, 2000- 5 (DEM)  Commercial/scientific: thematic & topographic mapping, hydrology, oil and gas exploration,

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table C - Operational airborne SAR sensors and specifications

Sensor, operating agency and date, application area Flying height (km) Swath Frequency Spatial Incidence width Imaging modes resolution angle (°)

Nation (km) (m)

infrastructure planning, crop monitoring, forestry, fuel mapping UAVSAR 13.8 16 L- full pol 2 rng NASA JPL  Differential interferometry for investigating dynamic phenomena (earthquakes, volcanoes, deformation, vegetation, soil moisture, ice/glaciers, oceanography)

STAR3i/IFSARE (Interferometric SAR – Elevation) 12.2 10 X-HH 3 45 ERIM, USA, 1992- 2.5-10 DEM  Military and civil use: interferometric mapping, DEM (abs V.Acc 3) generation

SOUTH AMERICA

SARAT 9 L-band polarimetry 3x0.4 23-69 CONAE, Argentina HH,HV,VH,VV  Test bed for SAOCOM satellite and integration with multi-frequency SAR data for extracting physical

information ARGENTINA Orbisar-RFP (Radar for Foliage Penetration) X- and P-band InSAR

OrbiSat, Brazil

 Cartographic products, including DTMs, ortho- images, contour maps, topographic maps for

BRAZIL applications in mining, gas and oil, defence, environment, energy

US MILITARY DCS (Data Collection System) 6.1 X- full pol 1.2 45 ERIM, US Air Force Ku-VV  -Single-pass interferometry

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table C - Operational airborne SAR sensors and specifications

Sensor, operating agency and date, application area Flying height (km) Swath Frequency Spatial Incidence width Imaging modes resolution angle (°)

Nation (km) (m)

ASARS-2A (Advanced SAR System) Payloads: electro-optical, IR and SAR Onboard U2 aircraft imagers, film camera, signals intelligence US Air Force equipment  Military reconnaissance & surveillance, target detection, damage assessment, disaster survey

P-3/SAR UWB (0.35 GHz) VV, VH, HH, HV ERIM, Navy L-VV, VH, HH, HV C-VV, VH, HH, HV X-VV, VH, HH, HV

SAR onboard RC-7 ARL aircraft Payloads: communications, signals and 1.8 US Military imagery intelligence  Military intelligence gathering Phased-array radar onboard E-8C JSTARS aircraft Multi-mode SAR system Antenna US Air Force Wide Area Surveillance (WAS) tilted to  Ground surveillance & moving target detection Moving Target Indicator (MTI) either side 120° FOV SAR onboard MQ-1 Predator UAV 7.62 0.3-1 US Air Force, 1995-  Military surveillance and reconnaissance, intelligence gathering, weapons delivery

SAR onboard RQ-4A Global Hawk UAV 19.8 UAV equipped with electro-optical, IR and US Air Force SAR imagers  Military intelligence, moving target detection, SAR MTI system, X-band Spotlight mode damage assessment 10 Stripmap mode 0.3-1.8 37 Wide-area mode 6

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table D - Decommissioned SAR sensors

Table D - Decommissioned SAR sensors

AIRBORNE

Sensor, operating agency and date, application area Flying height (km) Swath Frequency Spatial Incidence width Imaging modes resolution angle (°)

Nation (km) (m) AIRSAR (Airborne SAR) and TOPSAR (Topographic SAR) 8 10-15 C-, L- and P- Polarimetric 10 0-70 NASA JPL, USA 4.6 Cross-track Interferometric (XTI)

1993-2000 TOPSAR Along-track Interferometric (ATI) USA

SATELLITE

Sensor, operating agency, launch, application area Orbit & altitude Swath Frequency Spatial Incidence (km) width Imaging modes resolution angle (°)

Nation Inclination angle (°) (km) (m) Target revisit time X-BAND

IGS-1B, IGS-4B 486-491 km 1-3

(Information Gathering Satellites) 97.3° 1B 2003-2007, 4B 2007-2010

JAPAN  Military surveillance C-BAND ERS-1 (Earth Resources Satellite) Sun-synch polar 100 C-VV 30x26.3 23 ESA, 1991-2000  Earth observation, meteorology, topographic ITALY mapping

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table D - Decommissioned SAR sensors

Sensor, operating agency, launch, application area Orbit & altitude Swath Frequency Spatial Incidence (km) width Imaging modes resolution angle (°)

Nation Inclination angle (°) (km) (m) Target revisit time ERS-2 800 km 100 SAR image mode C-VV 26 20-26 ESA, 1995-2011 98.5° 5 SAR wave mode Right looking -Earth observation 35 days Wind scatterometer mode

ENVISAT ASAR (Advanced SAR) 800 km 100 Image mode (HH or VV) 30 15-45 ESA, 2002-2012 98.5° 100 Alternating pol (VV+HH or VV+VH or 30 Right looking  Earth observation: land, sea, ice, ocean monitoring 35 days HH+HV) & surveillance 400 Wide swath mode (HH or VV) 150 Global monitoring mode (HH or VV) 400 Wave mode (HH or VV) 1000

5 30 S-BAND Almaz-1 270 km 40 HH 10-15 25-60

1991-1992 72.7° Left and  Oceanography, geology, cartography & geophysics, right looking climate change, forestry,

RUSSIA  Agriculture, ecology

Lacrosse 1-5/Onyx 666 km 5 satellite program 1

NRO, 1988-2011 57-68°  Military reconnaissance USA

L-BAND JERS-1 (Japanese Earth Resources Satellite) 570 km 75 L-HH 18 32-38

JAXA, 1992-1998 98.5°

 Tropical & boreal forest mapping 44 days JAPAN

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 19

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications Table D - Decommissioned SAR sensors

Sensor, operating agency, launch, application area Orbit & altitude Swath Frequency Spatial Incidence (km) width Imaging modes resolution angle (°)

Nation Inclination angle (°) (km) (m) Target revisit time ALOS PALSAR 691 km L- Multiple modes (Phase Array L-band SAR) 98.16° 70 Fine Beam Single HH 10 34.3-41.5 JAXA, 2006-2011 46 days 70 Fine Beam Dual HH+HV 20 34.3-41.5  Earth observation 30 Quad pol HH+HV+VH+VV 30 21.5 350 Wide Beam HH 100 18-43 Right looking JianBing-5 (JB 5-1/ 1) 628 km 40 Spotlight 5 2006-2010 97.8 ° 100 ScanSAR 20 Dual use  Military: intelligence gathering, surveillance and

reconnaissance CHINA  Earth observation: land survey, disaster forecasting, crop yield evaluation, urban planning MULTI-FREQUENCY SIR-C/X-SAR (Shuttle Imaging Radar) 215 15-90 C- and L- full pol (HH,HV,VH,VV) 10-200 49 NASA JPL, 1994 57° X-VV Multi-ang

 Experimental program for multi-freq/pol/ang SAR 2x11 day missions 15-40 pointing for extracting physical information capability USA

SRTM (Shuttle Radar Topography Mission) 233 km 225 SIR-C HH+VV 30-90 17-65 NASA JPL, USA and DLR, Germany 57° X-SAR HH+VV (abs v.acc 16 Feb 2000 11 day mission m)

 Near-global DEM generation USA & GERMANY & USA

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