UniSat (original) (raw)

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UniSat

Unisat 6
Credit: Manufacturer Image

Italian technology satellite developed by the GAUSS (Gruppo di Astrodinamica dell' Universita degli Studi 'la Sapienza') in Roma. Technology satellite for GAUSS (La Sapienza University of Rome), Italy. Launched 2000-2006.

Status: Operational 2000. First Launch: 2000-09-26. Last Launch: 2014-06-19. Number: 5 . Gross mass: 12 kg (26 lb).

Unisat was financed by ASI and MURST (Ministero dell'Universtia e della Ricerca Scientifica e Tecnologica). The first carried NiMH batteries, a magnetometer, and a payload consisting of a space debris sensor and a camera. Later models were used to test customer equipment and deploy cubesats or Pocket-PUCP's.

More at: UniSat.

Subtopics

UniSat 5 Technology satellite for GAUSS Srl, Italy. Launched 2013.

UniSat 6 Technology satellite for GAUSS Srl, Italy. Launched 2014.

UniSat 7 Technology satellite for GAUSS Srl, Italy.

Family: Technology, Technology satellite. Country: Italy. Launch Vehicles: R-36M 15A14, R-36M2 15A18M, Dnepr. Launch Sites: Baikonur, Baikonur LC109. Agency: La Sapienza, GAUSS. Bibliography: 2, 552, 554.

Photo Gallery

	UniSat 1Credit: Manufacturer Image

	Unisat-5Credit: Manufacturer Image

	UniSat 7Credit: Manufacturer Image

2000 September 26 - . 10:05 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC109. Launch Pad: LC109/95. LV Family: R-36M. Launch Vehicle: Dnepr.

UniSat - . Mass: 10 kg (22 lb). Nation: Italy. Agency: Makeyev bureau. Manufacturer: la Sapienza. Class: Technology. Type: Navigation technology satellite. Spacecraft: UniSat. USAF Sat Cat: 26547 . COSPAR: 2000-057C. Apogee: 670 km (416 mi). Perigee: 643 km (399 mi). Inclination: 64.56 deg. Period: 97.78 min.
Experimental satellite developed by the GAUSS (Gruppo di Astrodinamica dell' Universita degli Studi 'la Sapienza') in Roma. Unisat was financed by ASI and MURST (Ministero dell'Universtia e della Ricerca Scientifica e Tecnologica). It carried NiMH batteries, a magnetometer, and a payload consisting of a space debris sensor and a camera.

2002 December 20 - . 17:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC109. Launch Pad: LC109/95. LV Family: R-36M. Launch Vehicle: Dnepr.

UniSat 2 - . Mass: 10 kg (22 lb). Nation: Italy. Agency: Makeyev bureau. Manufacturer: La Sapienza. Class: Technology. Type: Navigation technology satellite. Spacecraft: UniSat. USAF Sat Cat: 27608 . COSPAR: 2002-058D. Apogee: 667 km (414 mi). Perigee: 636 km (395 mi). Inclination: 64.60 deg. Period: 97.80 min.

2004 June 29 - . 06:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC109. Launch Pad: LC109/95. LV Family: R-36M. Launch Vehicle: Dnepr.

Unisat 3 - . Mass: 12 kg (26 lb). Nation: Italy. Agency: La Sapienza. Class: Technology. Type: Navigation technology satellite. Spacecraft: UniSat. USAF Sat Cat: 28373 . COSPAR: 2004-025H. Apogee: 800 km (490 mi). Perigee: 684 km (425 mi). Inclination: 98.30 deg. Period: 99.80 min.

2013 November 21 - . 07:10 GMT - . Launch Site: Dombarovskiy. Launch Pad: xxx. LV Family: R-36M. Launch Vehicle: Dnepr.

Unisat-5 - . Mass: 19 kg (41 lb). Nation: Italy. Class: Technology. Type: Technology satellite. Spacecraft: Unisat. USAF Sat Cat: 39421 . COSPAR: 2013-066F. Apogee: 636 km (395 mi). Perigee: 592 km (367 mi). Inclination: 97.78 deg. Period: 96.97 min.
Technology satellite for the University of Rome. It carried a further eight tiny satellites within it, and one of those (PUCP-Sat) carried a further nested satellite, Pocket-PUCP. Most of the subsatellites were ejected from Unisat-5 between 08:10 and 08:25 GMT on November 21.

2014 June 19 - . 19:11 GMT - . Launch Site: Dombarovskiy. LV Family: R-36M. Launch Vehicle: Dnepr.

Unisat 6 - . Mass: 26 kg (57 lb). Nation: Italy. Spacecraft: Unisat. USAF Sat Cat: 40012 . COSPAR: 2014-033C. Apogee: 699 km (434 mi). Perigee: 613 km (380 mi). Inclination: 97.97 deg. Period: 97.86 min. Satellite by GAUSS Srl to test customer equipment and deploy four cubesats..

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