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YAHSAT 1A

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YAHSAT 1A is classified as:


NORAD ID: 37393
Int'l Code: 2011-016B
Perigee: 35,790.4 km
Apogee: 35,797.5 km
Inclination: 0.0 °
Period: 1,436.1 minutes
Semi major axis: 42164 km
RCS: 10 m2 (large)
Launch date: April 22, 2011
Source: United Arab Emirates (UAE)

The high-powered Yahsat 1A satellite will be located in geosynchronous orbit along the equator at 52.5 degrees east longitude, putting the craft in range of communications customers across the Middle East, Africa, Europe and Southwest Asia. Operated by Al Yah Satellite Communications Co. of Abu Dhabi, Yahsat 1A will provide direct-to-home television programming, secure Ka-band communications capacity for government and military applications in the United Arab Emirates and other nations. Yahsat 1A will also support communications links for corporate data networks and Internet trunking, according to the satellite operator. Weighing 13,150 pounds (5,965 kg) at launch, Yahsat 1A is based on the Eurostar E3000 satellite bus from Astrium. Thales Alenia Space of France built Yahsat 1A's Ku-band, C-band and Ka-band communications payload. Yahsat 1A is designed to work in space for more than 15 years.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 37393U 11016B   15150.08841230  .00000103  00000-0  00000+0 0  9995
2 37393 000.0145 291.0759 0000847 136.2542 264.2721 01.00271144 15103

Source of the keplerian elements: AFSPC

N2YO: 297