Official name UNISAT 2
Alternative name Unisat-2
Cospar ID 2002-058D
Norad ID 27608
Launch date 2002-12-20
Launch site TTMTR
Launch vehicle Dnepr
Country/Organization Italy
Type application Technology
Operator GAUSS (La Sapienza University of Rome)
RCS size MEDIUM
Decay date ON ORBIT
Period (min) 97.25
Inclination (deg) 64.55
Perigee (km) 618
Apogee (km) 636
Eccentricity 0.0143540669856459
Mean motion (revs. per day) 14.8071979434447
Semi-Major axis (km) 7005.135
Raan (deg) 238.2512
Arg of perigee (deg) 106.3257
Shape Box + 1 Arm
Mass (kg) 12
Height (m) 0.3
Width (m) 0.2
Depth (m) 0.2
Span (m^2) 0.8
Contractors GAUSS (La Sapienza University of Rome)
Propulsion None
Configuration Octagonal prism
Power Solar cells, batteries

UniSat (University Satellite) are a series of small (~12 kg) satellites developed at the Scuola di Ingegneria Aerospaziale by the Gruppo di Astrodinamica dell'Università degli Studi “La Sapienza University of Rome” (GAUSS) to perform technology experiments and to check the use of non space rated equipment in space.

The UNISAT program has been the first university program in Italy intended for promoting the use of commercial technologies in the aerospace field, performing in-orbit tests of up-to-date technologies, with short development times and with a remarkable cost reduction.

In the first prototype UNISAT-1, flown on board a Dnepr launch vehicle on September 26th 2000, the technological issues prevailed over scientific motivations as the main goal was the acquisition of space hardware manufacturing experience for next missions. The technological payloads hosted on-board the spacecraft (terrestrial technology solar panels, commercial battery packs assembly, ad-hoc developed attitude control hardware) were flown following this design philosophy. Once flight tested, these experimental payloads were also integrated in the UNISAT-2 bus (launched in December 2002).

UNISAT 3 carries a magnetometer and triple junction solar cells.

The launch of UNISAT 4 was not successful, as the Dnepr failed 86 sec after launch.

Satellite COSPAR Date LS Launch Vehicle Remarks
UNISAT 2000-057C 2000-09-26 TTMTR Dnepr with MegSat 1, SaudiSat 1a, SaudiSat 1b, Tiungsat 1
UNISAT 2 2002-058D 2002-12-20 TTMTR Dnepr with LatinSat A, LatinSat B, Rubin 2, SaudiSat 1c, TrailBlazer-2001-Dummy
UNISAT 3 2004-025H 2004-06-29 TTMTR Dnepr with DEMETER, SaudiSat 2, SaudiComsat 1, SaudiComsat 2, LatinSat C, LatinSat D, AMSAT-Echo