Iridium (satellite)In one 13-day period (late-March to early-April 1998) they successfully put 14 satellites into orbit. The most recent launches took place in 2002 when a total of seven spare satellites were launched. Over the years several Iridium satellites have ceased to work and tumbled out of control, some have reentered the atmosphere while other partially functional satellites have remained in orbit. The satellites orbit from pole to pole with an orbit of roughly 100 minutes.
Orbital velocity of the satellites is approximately 17,000 mph (27,000 km/h). The inventors of the system had previously worked on a government study in the late 1980s that showed that microwave cross links were simpler and had fewer risks than optical cross links.
Although optical links could have supported a much greater bandwidth and a more aggressive growth path, microwave cross links were favored because the bandwidth was more than sufficient for the desired system. These satellites will incorporate features such as data transmission which were not emphasized in the original design.
Iridium simply waits until the desired RAAN (i.e., the desired orbital plane) is reached and then raises the spare satellite to the standard altitude, fixing its orbital plane with respect to the constellation. Satellites are in low Earth orbit at a height of approximately 485 mi (781 km) and inclination of 86.4°.
Although this saves substantial amounts of fuel, this can be a time-consuming process. Iridium is currently engaged in studies to build and launch a second generation of satellites, consisting of 66 satellites and six spares. It was found that this design did not have enough bandwidth in the space-based backhaul to upload each satellite quickly and reliably over the poles.
The earth s equatorial bulge causes the orbital right ascension of the ascending node (RAAN) to precess at a rate that depends mainly on the period and inclination. Late in the project an extra processor ( SAC ) was added to perform resource management and phone call processing. The cellular look down antenna has 48 spot beams arranged as 16 beams in three sectors.
At its peak during the launch campaign in 1997 and 1998, Motorola produced a new satellite every 4.3 days, with the throughput time of a single satellite being 21 days. Motorola used launch vehicles from three companies from three different countries — the Delta II from McDonnell Douglas; the Proton K from Krunichev in Russia; and the Long March IIC from China Aerospace Science and Technology Corporation. Such cross-links are unique in the satellite telephone industry, as other providers do not relay data between satellites. The original design envisioned a completely static 1960s dumb satellite with a set of control messages and time-triggers for an entire orbit that would be uploaded as the satellite passed over the poles.
A move can take several weeks, and consumes fuel which will shorten the satellite s expected service life. Significant orbital plane changes are normally very fuel-intensive, but orbital perturbations aid the process. not every plane has a spare satellite however the satellites can be moved to a different plane if required.
In recent press releases, Iridium Satellite LLC has stated that their second generation satellites would also use microwave, not optical, inter-satellite communications links. The over-the-pole orbital design produces seams where satellites in counter-rotating planes next to one another are travelling in opposite directions.
In August 2008, Iridium selected two companies — Lockheed Martin and Thales Alenia Space — to participate in the final phase of the procurement of the next generation satellite constellation, with the winner to be announced in mid-2009. The main patents on the Iridium system, U.S. Satellite manufacturing initiatives were also instrumental in the technical success of the system.
This system will be backward compatible with the current system. He created the technology necessary to mass-produce satellites on a gimbal, taking weeks instead of months or years and at a record low construction cost of only US$5 million per satellite.
However these satellites are not in active service. Iridium 28 failed in July 2008 and has been replaced with the in-orbit spare Iridium 95. At 16:56 UTC on February 10, 2009 Iridium 33 collided with the defunct Russian satellite, Kosmos-2251. Iridium Satellite LLC owns and operates the constellation and sells equipment and access to its services. The constellation requires 66 active satellites in orbit to complete its constellation and additional spare satellites are kept in-orbit to serve in case of failure.
Nevertheless, a parallel optical cross link option was carried through a critical design review, and ended when the microwave cross links were shown to support the size, weight and power requirements allocated within the individual satellite s budget. The four inter-satellite cross links on each satellite operate at 10 Mbit/s.
The Iridium satellite constellation is a large group of satellites used to provide voice and data coverage to satellite phones, pagers and integrated transceivers over Earth s entire surface. Cross-seam intersatellite link handoffs would have to happen very rapidly and cope with large Doppler shifts; therefore, Iridium supports intersatellite links only between satellites orbiting in the same direction. The satellites each contain seven Motorola/Freescale PowerPC 603E processors running at roughly 200 MHz Processors are connected by a custom backplane network.
The original constellation of 66 satellites, plus six spares, was launched in 12 months and 12 days, between May 5, 1997, and May 17, 1998, with an astounding success rate of 15 out of 15 successful launches and all 72 satellites put into the intended orbits. Therefore, the design was scrapped in favor of a design that performed dynamic control of routing and channel selection late in the project, resulting in a one year delay in system delivery. Each satellite can support up to 1100 concurrent phone calls and weighs about 1,500 lb (680 kg). Owing to the highly reflective antennas, Iridium satellites cause a phenomenon known as Iridium flares, watched by enthusiasts and sometimes visible in daylight. Spare satellites are usually held in a 414 mi (666 km) storage orbit.
Patents 5,410,728 and 5,604,920, are in the field of satellite communications, and the manufacturer generated several hundred patents protecting the technology in the system. The current plan is to begin launching new satellites in 2014. The existing constellation of satellites is expected to remain operational until at least 2014, with many satellites expected to remain in service until the 2020s.
Iridium 33 was in active service when the accident took place but was one of the oldest satellites in the constellation, having been launched in 1997. Iridium moved one of its in-orbit spares to replace the destroyed satellite, completing the move on March 4, 2009. A video has been produced to show the relationship of the two satellites as they collided. . Satellites communicate with neighboring satellites via Ka band intersatellite links.
This design means that there is excellent satellite visibility and service coverage at the North and South poles, where there are few customers. Iridium satellites have an inclination of 86.4°, so like every satellite in a prograde (inclination < 90°) orbit, their equator crossings steadily precess westward. A spare Iridium satellite in the lower storage orbit has a shorter period so its RAAN moves westward more quickly than the satellites in the standard orbit.
Each satellite can have four intersatellite links: two to neighbors fore and aft in the same orbital plane, and two to satellites in neighboring planes to either side. Iridium is planning a new generation of satellites with improved bandwidth to be operational by 2016.
Motorola made a key hire of the engineer who set up the automated factory for Apple s Macintosh. One processor is dedicated to each cross-link antenna ( HVARC ), and two processors ( SVARC s) are dedicated to satellite control, one being a spare.