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Ikonos

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Ikonos

Status: Operational 1999. First Launch: 1999-04-27. Last Launch: 1999-09-24. Number: 2 . Gross mass: 726 kg (1,600 lb).

It carried a 1-m resolution panchromatic camera and a 4-m resolution color imager, with a 13 km swath width. Built on an LM-900 bus. 6 MR-103G 0.1N thrusters for attitude control.

Photo Gallery

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Ikonos Credit: Manufacturer Image

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• Ikonos 1 - . Mass: 726 kg (1,600 lb). Nation: USA. Agency: Martin. Class: Surveillance. Type: Civilian surveillance satellite. Spacecraft Bus: LM-900. Spacecraft: Ikonos.

  Tracking stations downrange did not pick up the spacecraft. It was later determined that the rocket nose fairing failed to separate four minutes after launch. The extra mass caused the vehicle to reenter over the South Pacific on the first partial orbit. Space Imaging's Ikonos 1 was to have been the first commercial imaging satellite with a high a resolution camera.

• Ikonos - . Mass: 726 kg (1,600 lb). Nation: USA. Agency: SpaceIm. Manufacturer: Lockheed. Class: Surveillance. Type: Civilian surveillance satellite. Spacecraft Bus: LM-900. Spacecraft: Ikonos. USAF Sat Cat: 25919 . COSPAR: 1999-051A. Apogee: 679 km (421 mi). Perigee: 678 km (421 mi). Inclination: 98.10 deg. Period: 98.30 min. Commercial / civilian high resolution (1 metre resolution) photograhic satellite..