Official name ITALSAT 2
Alternative name Italsat 2
Cospar ID 1996-044A
Norad ID 24208
Launch date 1996-08-08
Launch site FRGUI
Launch vehicle Ariane-44L H10-3
Country/Organization Italy
Type application Communication
RCS size LARGE
Decay date ON ORBIT
Period (min) 1428.81
Inclination (deg) 13.4
Perigee (km) 35534
Apogee (km) 35754
Eccentricity 0.00308607339243631
Mean motion (revs. per day) 1.00783169210742
Semi-Major axis (km) 42022.135
Raan (deg) 12.4146
Arg of perigee (deg) 125.5683
Shape Hex Poly + 2 Pan
Mass (kg) 1189.3
Height (m) 3.5
Width (m) 2.3
Depth (m) 2.3
Span (m^2) 23.98
Lifetime 6 years (#1), 8 years (#2)
Contractors Alenia Spazio
Equipment 9 (+6) Ka-band transponders (both), Ka-band propagation beacon (#1), L-band, Ku-band transponder
Propulsion R-4D-11
Configuration GeoBus (Italsat Bus)
Power 2 deployable solar arrays, batteries

Italy's first operational communications satellite was launched 15 January 1991 by an Ariane-44L H10 booster. Developed by a contractor team led by Alenia Spazio, Italsat carries ten active transponders plus five spares for 30/20 GHz and 50/40 GHz links with a capacity of 12,000 telephone circuits. The 900 kg (on-station) spacecraft consists of a rectangular bus 2.3 m by 2.7 m by 3.5 m and two solar panels with a total span of 21.8 m and more than 1.5 kW power. The design life for the first test vehicle is only five years, increased to 8 for the second Italsat. Italsat 2 was launched in 1996 by a Ariane-44L H10-3. It also carries ESA's first European Mobile Services (EMS) payload. Italsat 2 was undergoing environmental testing in France in late 1994. Italsat 1 is stationed at 13.2 degrees E, also be the home of Italsat 2.

The satellites were moved to graveyard orbits in January 2001 and July 2002 respectively.

Satellite COSPAR Date LS Launch Vehicle Remarks
ITALSAT 1 1991-003A 1991-01-15 FRGUI Ariane-44L H10 with Eutelsat-2 F2
ITALSAT 2 1996-044A 1996-08-08 FRGUI Ariane-44L H10-3 with Télécom 2D