Official name HOT BIRD 1
Alternative name Hotbird 1
Cospar ID 1995-016B
Norad ID 23537
Launch date 1995-03-28
Launch site FRGUI
Launch vehicle Ariane-44LP H10+
Country/Organization International
Type application Communication (Direct Broadcasting)
Operator Eutelsat
RCS size MEDIUM
Decay date ON ORBIT
Period (min) 1449.87
Inclination (deg) 12.61
Perigee (km) 36039
Apogee (km) 36073
Eccentricity 0.000471488795207455
Mean motion (revs. per day) 0.993192493120073
Semi-Major axis (km) 42434.135
Raan (deg) 25.5203
Arg of perigee (deg) 68.0873
Shape Hex Poly + 2 Pan
Mass (kg) 1068.38
Height (m) 2.2
Width (m) 2.5
Depth (m) 2.5
Span (m^2) 22.38
Contractors Aerospatiale
Equipment 16 (+8) Ku-band transponders
Propulsion S400
Configuration Spacebus-2000
Power 2 deployable solar arrays, batteries

The last of the Eutelsat 2 series spacecraft was modified for direct to home (DTH) broadcastingscheduled for launch in 1995 under the name Hot Bird 1. The satellite will be essentially the same as its predecessors, but the transponder output power will be increased from 50 W to 70 W.

The spacecraft wast procured directly from Aerospatiale and based on the Spacebus-2000 design. It supports 16 transponders (with eight spares) operating at 14/11 GHz and 70 W output power. In orbit the spacecraft spans 22.4 m across the two rectangular solar arrays which generate up to 3.5 kW. Hot Bird 1 employs one, 1.6 m diameter multifeed reflector.

Satellite COSPAR Date LS Launch Vehicle Remarks
HOT BIRD 1 1995-016B 1995-03-28 FRGUI Ariane-44LP H10+ with Brasilsat B2