Intelsat 23

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Intelsat 23
Start date October 14, 2012, 10:37 UTC
Launcher Proton-M / Bris-M
Launch site Baikonur, launch pad 81/24
COSPAR-ID : 2012-057A
Takeoff mass 3,200 kg
Empty mass 1,503 kg
Manufacturer Orbital Sciences Corporation
Satellite bus GEOStar-2
lifespan 15 years (planned)
Stabilization Three-axis
operator Intelsat
Playback information
Transponder 24 C and 15 Ku bands
Transponder performance * 19-for-15 TWTA (Ku-Band) * two 16-for-12 TWTA (C-Band)
Bandwidth * 72, 77 and 112 MHz (Ku-band) * 36, 41, 72 and 77 MHz (C-band)
EIRP *> 44.0 dBW (Ku band) *> 31.7 dBW (C band)
Others
Electrical power 4.8 kW
Power storage two lithium-ion batteries.
position
First position 53 ° west
drive Dual-fuel apogee motor , as well as hydrazine drives for position control
List of geostationary satellites

Intelsat 23 is a commercial communications satellite owned by the satellite operator Intelsat .

He was a on October 14, 2012 Proton-M / Briz-M - carrier rocket from the Baikonur Cosmodrome in a geostationary brought orbit and to Intelsat 707 replace. After a little over 9 minutes and 41 seconds of flight time, the upper stage with the satellite was separated from the rocket and the rocket was placed in the intended position after 9 hours and 30 minutes.

The three-axis stabilized satellite with 15 Ku-band - and 24 C-band - transponders m and two 2.5 x 2.7 and 1.3 x 1.65 m equipped a large antennas and to the position of 53 ° West African , Western Europe, the Caribbean, certain islands in the Atlantic and Pacific, as well as North and South America with a wide range of communication services. It was based on the Geostar-2 - satellite bus of Orbital Sciences Corporation (OSC) built and has a design life of 15 years.

Web links

Individual evidence

  1. a b Thomas Weyrauch: Intelsat 23 started on Proton-M. October 14, 2012, accessed September 4, 2012 .