JERS-1 was launched in February 1992 by NASDA
(Japanese Space Agency). This satellite
carries a L-band SAR and an optical sensor for generation of
global data set in order to survey
resources and to establish an integrated Earth observation
system.
JERS-1 Orbit
Type | Sun-Synchronous |
Altitude | 568 km |
Inclination | 97.7 deg |
Period | 96 min |
Repeat Cycle | 44 days |
Sensors
- SAR (Synthetic Aperture Radar)
- OPS (Optical Sensor)
JERS-1 SAR Instrument Characteristics
Frequency | 1.275 GHz (L band) |
Polarisation | Linear HH |
Bandwidth | 15.55 MHz |
Incidence angle | 35o nominal |
Swath width | 75 km |
Resolution | 18 m (azimuth, 3 looks), 18 m (range) |
Back to Main Index
|
|