AKO Polyot

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AKO Polyot

Part of Polyot

Russian manufacturer of rockets, Omsk, Russia.

AKA: Polyot. Location: Omsk.

Country: Russia. Launch Vehicles: Kosmos 65S3, R-14U, Kosmos 3, Kosmos 11K65, Kosmos 11K65M, K65M-R, Vertikal' K65UP, K65M-RB, Kosmos 65MP.

1997 April 17 - . 13:03 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.

Cosmos 2341 - . Mass: 825 kg (1,818 lb). Nation: Russia. Agency: MO. Manufacturer: AKO Polyot. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Parus. USAF Sat Cat: 24772 . COSPAR: 1997-017A. Apogee: 1,014 km (630 mi). Perigee: 977 km (607 mi). Inclination: 82.90 deg. Period: 105.00 min. Military navigation satellite. Positioned in plane 2 of constellation. Signals at 149.91 and 399.76 MHz..

1998 December 10 - . 11:57 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.

Nadezhda 5 - . Payload: Tsikada-Kospas. Mass: 820 kg (1,800 lb). Nation: Russia. Agency: MO. Manufacturer: AKO Polyot. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Nadezhda. USAF Sat Cat: 25567 . COSPAR: 1998-072A. Apogee: 1,013 km (629 mi). Perigee: 974 km (605 mi). Inclination: 83.00 deg. Period: 105.00 min.

1998 December 24 - . 20:02 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.

Cosmos 2361 - . Mass: 825 kg (1,818 lb). Nation: Russia. Agency: MO. Manufacturer: AKO Polyot. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Parus. USAF Sat Cat: 25590 . COSPAR: 1998-076A. Apogee: 1,013 km (629 mi). Perigee: 967 km (600 mi). Inclination: 82.90 deg. Period: 104.90 min. A Parus navigation satellite in the same orbital plane as Cosmos 2233..

1998 December 30 - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton-K/DM-2.

Cosmos 2362 - . Mass: 1,370 kg (3,020 lb). Nation: Russia. Agency: MOM. Manufacturer: AKO Polyot. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 25593 . COSPAR: 1998-077A. Apogee: 19,177 km (11,916 mi). Perigee: 19,082 km (11,856 mi). Inclination: 63.50 deg. Period: 675.70 min.

Cosmos 2364 - . Mass: 1,370 kg (3,020 lb). Nation: Russia. Agency: MOM. Manufacturer: AKO Polyot. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 25595 . COSPAR: 1998-077C. Apogee: 19,135 km (11,889 mi). Perigee: 19,125 km (11,883 mi). Inclination: 63.50 deg. Period: 675.70 min.

Cosmos 2363 - . Mass: 1,370 kg (3,020 lb). Nation: Russia. Agency: MOM. Manufacturer: AKO Polyot. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 25594 . COSPAR: 1998-077B. Apogee: 19,163 km (11,907 mi). Perigee: 19,097 km (11,866 mi). Inclination: 63.50 deg. Period: 675.70 min.

1999 August 26 - . 12:02 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.

Cosmos 2366 - . Mass: 825 kg (1,818 lb). Nation: Russia. Agency: MO. Manufacturer: AKO Polyot. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Parus. USAF Sat Cat: 25892 . COSPAR: 1999-045A. Apogee: 1,007 km (625 mi). Perigee: 963 km (598 mi). Inclination: 82.90 deg. Period: 104.80 min.

2000 June 28 - . 10:37 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.

Nadezhda - . Payload: Tsikada-Kospas. Mass: 825 kg (1,818 lb). Nation: Russia. Agency: MO. Manufacturer: AKO Polyot. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Nadezhda. USAF Sat Cat: 26384 . COSPAR: 2000-033A. Apogee: 712 km (442 mi). Perigee: 686 km (426 mi). Inclination: 98.14 deg. Period: 98.66 min. Nadezhda navigation/search and rescue satellite. This represented the first sun-synchronous launch from Plesetsk..

2000 October 13 - . 14:12 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/24. LV Family: Proton. Launch Vehicle: Proton-K/DM-2.

Cosmos 2374 - . Payload: Glonass s/n 83. Mass: 1,415 kg (3,119 lb). Nation: Russia. Agency: MO. Manufacturer: AKO Polyot. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 26564 . COSPAR: 2000-063A. Apogee: 19,136 km (11,890 mi). Perigee: 19,124 km (11,883 mi). Inclination: 64.60 deg. Period: 675.70 min.
Three navigation satellites for the GLONASS system were launched by a single Proton-K/Blok DM-2 upper stage into an initial 160 km x 64.8 deg parking orbit. The Blok DM-2 made two burns to maneuver into a 19120 x 19120 km x 64.8 deg orbit and deployed the three satellites about four hours after launch.

Cosmos 2376 - . Payload: Glonass s/n 88. Mass: 1,415 kg (3,119 lb). Nation: Russia. Agency: MO. Manufacturer: AKO Polyot. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 26566 . COSPAR: 2000-063C. Apogee: 19,278 km (11,978 mi). Perigee: 18,982 km (11,794 mi). Inclination: 64.50 deg. Period: 675.70 min.

Cosmos 2375 - . Payload: Glonass s/n 87. Mass: 1,415 kg (3,119 lb). Nation: Russia. Agency: MO. Manufacturer: AKO Polyot. Class: Navigation. Type: Navigation satellite. Spacecraft: Glonass. USAF Sat Cat: 26565 . COSPAR: 2000-063B. Apogee: 19,136 km (11,890 mi). Perigee: 19,124 km (11,883 mi). Inclination: 64.60 deg. Period: 675.70 min.

2001 June 8 - . 15:08 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.

Cosmos 2378 - . Mass: 825 kg (1,818 lb). Nation: Russia. Agency: MO. Manufacturer: AKO Polyot. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: KAUR-1. Spacecraft: Parus. USAF Sat Cat: 26818 . COSPAR: 2001-023A. Apogee: 1,011 km (628 mi). Perigee: 961 km (597 mi). Inclination: 82.90 deg. Period: 104.80 min.
Launch delayed from April 26/27. Parus class navigation satellite, placed initially in a 150 x 1000 km transfer orbit; the second stage of the Kosmos-3M ignited again for a short 11 second burn to put the satellite in its final orbit. This was the first Kosmos-3M flight since a failure in November 2000.

2002 November 28 - . 06:07 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.

Rubin-3-DSI - . Mass: 80 kg (176 lb). Nation: Russia. Agency: NCST. Manufacturer: AKO Polyot, Bremen. Class: Technology. Type: Navigation technology satellite. Spacecraft: Rubin. USAF Sat Cat: 27561 . COSPAR: 2002-054C. Apogee: 748 km (464 mi). Perigee: 687 km (426 mi). Inclination: 98.20 deg. Period: 99.10 min.
Delayed from September 12, October 29. Rubin-3-DSI, with a mass of 45 kg, was built by PO Polyot of Omsk (builders of the Kosmos-3M) and OHB System of Bremen. It remained attached to the booster final stage and measured the launch vehicle environment and performance

2005 October 27 - . 06:52 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.

Sinah-1 - . Mass: 160 kg (350 lb). Nation: Iran. Agency: AKO Polyot. Class: Surveillance. Type: Civilian surveillance satellite. Spacecraft: Sterkh. USAF Sat Cat: 28893 . COSPAR: 2005-043D. Apogee: 705 km (438 mi). Perigee: 682 km (423 mi). Inclination: 98.20 deg. Period: 98.60 min.
First Iranian satellite, with an experimental surveillance camera payload. It may have used the Russian Polyot enterprise's Sterkh satellite bus. The same bus was to be used in future Nadezhda satellites. The Strekh bus was said to accomodate 80-100 kg satellites, and be 1.0 m high and 0.4 m in diameter, with a design life of 5 years. Sinah was 160 kg, and 0.8 x 1.3 x 1.6 m in dimensions. Or it may have been a version of the previously-announced satellite dubbed Mesbah-2.

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