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Detailed information about IRIDIUM 62 satellite

Designator id: 1998-021A

Description of IRIDIUM 62 Satellite:

Iridium 62 was part of a planned commercial communications network comprised of a constellation of 66 LEO spacecraft. The system will use L-Band to provide global communications services through portable handsets. A total of 125 spacecraft will be built by Lockheed for more than $700M. Commercial service is planned to begin in 1998. The system will employ 15-20 ground stations with a master control complex in Landsdowne, VA, a backup in Italy, and a third engineering center in Chandler, AZ. The spacecraft was 3-axis stabilized, with a hydrazine propulsion system. It had 2 solar panels with 1-axis articulation. The system employed L-Band using FDMA/TDMA to provide voice at 4.8 kbps and data at 2400 bps with 16 dB margin. Each satellite had 48 spot beams for Earth coverage and used Ka-Band for crosslinks and ground commanding.

Technical data:

Launch Date: 1998-04-07
Launch Vehicle: Proton-K
Launch Site: Kourou, French Guiana

Funding Agencies:

Iridium (United States)



Source: Nasa

Two Line Element Set (TLE):
1 25285U 98021A   12339.11828007  .00002076  00000-0  73379-3 0   917
2 25285 086.3960 196.0913 0002181 083.8897 276.2716 14.34234841767656

Last TLE update on :2012-12-04

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