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Reflektor

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Reflektor

Status: Operational 2001. First Launch: 2001-12-10. Last Launch: 2001-12-10. Number: 1 . Gross mass: 6.00 kg (13.20 lb). Height: 1.40 m (4.50 ft). Span: 0.50 m (1.64 ft).

The satellite consisted of four triangular fins on a square base plus a deployable boom, with an array of laser retroreflectors. The satellite was 1.4 m long and 0.5 m wide but only 6 kg in mass. It was used to calibrate laser imaging systems and other optical sensors.

Photo Gallery

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Reflektor Credit: Manufacturer Image

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Reflektor Credit: Manufacturer Image

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Reflektor Credit: Manufacturer Image

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• Reflektor - . Mass: 8.00 kg (17.60 lb). Nation: Russia. Agency: RAKA. Manufacturer: NII KP. Class: Technology. Type: Navigation technology satellite. Spacecraft: Reflektor. USAF Sat Cat: 27005 . COSPAR: 2001-056E. Apogee: 1,012 km (628 mi). Perigee: 985 km (612 mi). Inclination: 99.20 deg. Period: 105.10 min.

  The 8 kg Reflektor was built by NII KP in Russia for space debris studies in a joint experiment with the Air Force Research Lab. The satellite consisted of of four triangular fins on a square base plus a deployable boom, with an array of laser retroreflectors. The satellite was 1.4 m long and 0.5 m wide but only 6 kg in mass. It will be used to calibrate laser imaging systems and other optical sensors.