Official name ASTRA 1C
Alternative name Astra 1C
Cospar ID 1993-031A
Norad ID 22653
Launch date 1993-05-12
Launch site FRGUI
Launch vehicle Ariane-42L H10
Country/Organization Luxembourg
Type application Communication (Direct Broadcasting)
Operator SES
RCS size LARGE
Decay date ON ORBIT
Period (min) 1456.9
Inclination (deg) 12.32
Perigee (km) 36172
Apogee (km) 36214
Eccentricity 0.00058022269499627
Mean motion (revs. per day) 0.988400027455556
Semi-Major axis (km) 42571.135
Raan (deg) 28.3769
Arg of perigee (deg) 46.4049
Shape Hex Poly + 2 Pan
Mass (kg) 1684.84
Height (m) 4.3
Width (m) 2.7
Depth (m) 2.7
Span (m^2) 20.98
Lifetime 12 years
Contractors Hughes
Equipment 24 Ku-band transponders
Propulsion R-4D-11 (#1C), R-4D-11-300 (#1D)
Configuration HS-601
Power 2 deployable solar arrays, batteries

With its constellation of Astra spacecraft, Société Européenne des Satellites (SES) of Luxembourg is delivering analog as well as digital television and radio services across Europe.

SES ordered its first Hughes HS-601 satellite, called Astra 1C, in late 1990, after a six-month competitive bidding process. That was followed in late 1991 by an order for a second spacecraft, Astra 1D.

The Hughes' 601 satellite was designed for the higher-power missions of the 1990s. The model was introduced in 1987 to meet anticipated requirements for high-power, multiple-payload satellites for such uses as direct television broadcasting to small antennas, mobile communications, and private business networks.

The Astra satellites are similar in appearance to other 601 models, with each having a cube-shaped body and two solar array wings oriented along its north-south axis and the antennas located on the east-west axis.

All the satellites operate in Ku-band and use traveling-wave tube amplifiers (TWTAs) for power. On Astra 1C and 1D, the TWTAs provide 63 Watts each;

Astra 1C ans 1D each carry 18 operating transponders and six spares.

The satellites enable SES to provide analog and digital television programs together. Most operate at 19.2 degrees East longitude. On Astra 1C, the 18 transmission frequencies can be selected on-orbit from 34 possibilities. On Astra 1D and 1E, the on-orbit transmission frequency selection is increased to 66 possibilities.

The 1C and 1D satellites each measure 7.4 meters across with antennas deployed and 21 meters long from the tip of one three-panel solar array wing to the tip of the other. These solar arrays generate a combined 3500 Watts of electrical power, backed up by a 28-cell nickel-hydrogen battery for power during eclipse.

On the spacecraft, a flight-proven bipropellant propulsion system with an integral 490-Newton (110-lbf) Marquardt liquid apogee motor and 12 thrusters provides the impulse to achieve and maintain the orbit and attitude necessary for geosynchronous operation.

Satellite COSPAR Date LS Launch Vehicle Remarks
ASTRA 1C 1993-031A 1993-05-12 FRGUI Ariane-42L H10 with Arsene
ASTRA 1D 1994-070A 1994-11-01 FRGUI Ariane-42P H10+