Update on coms program


Figure 1. Artist’s rendering of COMS



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Figure 1. Artist’s rendering of COMS COMCOMSketch view of COMS.

(1) The COMS payload for earth observation



  • A Meteorological Imager with 5 channels in the range 0.55-12.5m, resolution of 1 km in 1 VIS channel, 4 km in 4 IR channels, 27 min for full disk imaging (proportionally less for limited areas). See instrument sheet in Annex A3.1.

  • An Geostationary Ocean Color Imager with 8 narrow-band channels in the range 400-865 nm for ocean color monitoring; resolution of 500 m over a limited coverage (2500 km x 2500 km). See instrument sheet in Annex A3.1.

(2) Data transmission from COMS

Raw data are transmitted to:


  • National Meteorological Satellite Center (NMSC/KMA), Korea Ocean Satellite Center (KOSC), and the Satellite Operation Center as backup.

      • Frequency of 1687 MHz, bandwidth of 6.0 MHz, RHCP/LHCP polarisation, 6 Mbps data rate.

After ground processing at NMSC and/or KOSC, data are re-transmitted to the users by:

  • HRIT (High Rate Information Transmission)

      • Frequencies of 1695.4 MHz; bandwidth of 5.2 MHz; Linear Polarization in horizontal direction

      • Antennas : diameters of 3.7 m, G/T ~ 11.1 dB/K, 3 Mbps information data rate;

  • LRIT (Low Rate Information Transmission)

      • Frequencies of 1692.14 MHz; bandwidth of 1 MHz; Linear Polarization in horizontal direction

      • Antennas : diameters of 1.2 m(down), G/T ~ 1.9 dB/K, 256 kbps data rate(TBC, more details in KMA-WP-03).

(3) Current Status of COMS (In-Orbit Test)

COMS has been launched from the Arianespace launch site in Kourou, French Guiana at 21:41 UTC on 26 June. After the launch, COMS has arrived its nominal position of geostationary orbit of 128.2E on 6 July and started the test mode on 10 July. The first MI visible image was acquired in 12 July and first IR images in 11 August after successful outgassing period.

In-Orbit Test has been performing in order to confirm the performance of the satellite system and payloads. The present steps for MI radiometric calibrations are generalized IR calibration, midnight effect correction, and slope averaging. And the step for MI INR (image navigation and registration) is the configuration parameter tuning and performance evaluation will be followed. COMS MI data service is expected to be started in early 2011.




Visible (0.55 - 0.8 μm)





Shortwave IR(3.50 - 4.0 μm)



Water Vapor (6.5 – 7.0 μm)





IR1(10.3 – 11.3 μm)



IR2(11.5 – 12.5 μm)


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