Replica of a first-generation Iridium satellite
|Manufacturer||Motorola (original constellation), Thales Alenia Space (NEXT constellation)|
|Country of origin||United States|
|Bus||LM-700 (original), EliteBus1000 (NEXT)|
|Launch mass||689 kilograms (1,519 lb)|
|Power||2 deployable solar panels + batteries|
|Regime||Low Earth orbit|
|Built||98 (original), 81 (NEXT)|
|Launched||95 (original), 75 (NEXT)|
|Operational||82 (76 in active service, 6 spares)|
|Maiden launch||Iridium 4, 5, 6, 7, 8 on 5 May 1997|
|Last launch||11 Jan 2019 |
The Iridium satellite constellation provides L-band voice and data information coverage to satellite phones, pagers and integrated transceivers over the entire Earth surface. Iridium Communications owns and operates the constellation, additionally selling equipment and access to its services. It was originally conceived by Bary Bertiger, Raymond J. Leopold and Ken Peterson in late 1987 (in 1988 protected by patents Motorola filed in their names) and then developed by Motorola on a fixed-price contract from July 29, 1993, to November 1, 1998, when the system became operational and commercially available.
The constellation consists of 66 active satellites in orbit, required for global coverage, and additional spare satellites to serve in case of failure. Satellites are in low Earth orbit at a height of approximately 781 km (485 mi) and inclination of 86.4°. Orbital velocity of the satellites is approximately 27,000 km/h (17,000 mph). Satellites communicate with neighboring satellites via Ka band inter-satellite links. Each satellite can have four inter-satellite links: one each to neighbors fore and aft in the same orbital plane, and one each to satellites in neighboring planes to either side. The satellites orbit from pole to same pole with an orbital period of roughly 100 minutes. This design means that there is excellent satellite visibility and service coverage especially at the North and South poles. The over-the-pole orbital design produces "seams" where satellites in counter-rotating planes next to one another are traveling in opposite directions. Cross-seam inter-satellite link hand-offs would have to happen very rapidly and cope with large Doppler shifts; therefore, Iridium supports inter-satellite links only between satellites orbiting in the same direction. The constellation of 66 active satellites has six orbital planes spaced 30° apart, with 11 satellites in each plane (not counting spares). The original concept was to have 77 satellites, which is where the name Iridium came from, being the element with the atomic number 77 and the satellites evoking the Bohr model image of electrons orbiting around the Earth as its nucleus. This reduced set of six planes is sufficient to cover the entire Earth surface at every moment.
Because of the shape of the original Iridium satellites' reflective antennas, the first generation satellites focus sunlight on a small area of the Earth surface in an incidental manner. This results in an effect called Iridium flares, where the satellite momentarily appears as one of the brightest objects in the night sky and can be seen even during daylight. Newer Iridium satellites do not produce flares.
The Iridium system was designed to be accessed by small handheld phones, the size of a cell phone. The omnidirectional antennas which are small enough to be mounted on such a phone, and the low battery power, are insufficient to allow the phone's radio waves to reach a satellite in geostationary orbit, 35,785 kilometres (22,236 mi) above the Earth, the normal orbit of communications satellites, in which the satellite appears stationary in the sky. In order for a handheld phone to communicate with them, the Iridium satellites are closer to the Earth, in low Earth orbit, about 781 kilometres (485 mi) above the surface. With an orbital period of about 100 minutes a satellite can only be in view of a phone for about 7 minutes, so the call is automatically "handed off" to another satellite when one passes beyond the local horizon. This requires a large number of satellites, carefully spaced out in polar orbits (see animated image of coverage) to ensure that at least one satellite is continually in view from every point on the Earth's surface. At least 66 satellites are required, in 6 polar orbits containing 11 satellites each, for seamless coverage.
The Iridium satellite constellation was conceived in the early 1990s, as a way to reach high Earth latitudes with reliable satellite communication services. Early calculations showed that 77 satellites would be needed, hence the name Iridium, after the metal with atomic number 77. It turned out that just 66 were required to complete the blanket coverage of the planet with communication services.
The first-generation constellation was developed by Iridium SSC, and financed by Motorola. The satellites were deployed in 1997-2002. All the satellites needed to be in orbit before commercial service could begin.
Iridium SSC employed a globally diverse fleet of rockets to get their 77 satellites into orbit, including launch vehicles (LVs) from the United States, Russia and China. 60 were launched to orbit on twelve Delta II LVs carrying five satellites each; 21 on three Proton-K/DM2 LVs with seven each, two on one Rokot/Briz-KM LVs carrying two; and 12 on six Long March 2C/SD LVs carrying two each. The total setup cost for the first-generation fleet was approximately US$5 billion.
The first test telephone call was made over the network in 1998, and full global coverage was complete by 2002. However, although the system met its technical requirements, it was not a success in the market. Insufficient market demand existed for the product at the price points on offer from Iridium as set by its parent company Motorola. The company failed to earn revenue sufficient to service the debt associated with building out the constellation and Iridium went bankrupt, one of the largest bankruptcies in US history at the time.
The constellation continued operation following the bankruptcy of the original Iridium corporation. A new entity emerged to operate the satellites and developed a different product placement and pricing strategy, offering communication services to a niche market of customers who required reliable services of this type in areas of the planet not covered by traditional geosynchronous orbit communication satellite services. Users include journalists, explorers, and military units.
The second-generation Iridium-NEXT satellites began to be deployed into the existing constellation in January 2017. Iridium Communications, the successor company to Iridium SSC, has ordered a total of 81 new satellites being built by Thales Alenia Space and Orbital ATK: 66 operational units, nine on-orbit spares, and six ground spares.
As of 2009, the original plan had been to begin launching new satellites in 2014.
The design was complete by 2010, and Iridium stated that the existing constellation of satellites would remain operational until Iridium NEXT is fully operational, with many satellites expected to remain in service until the 2020s, while the NEXT satellites would have improved bandwidth. The new system was to be backward-compatible with the current system. In June 2010, the winner of the contract was announced as Thales Alenia Space, in a $2.1 billion deal underwritten by Compagnie Française d'Assurance pour le Commerce Extérieur. Iridium additionally stated that it expected to spend about $800 million to launch the satellites and upgrade some ground facilities.
SpaceX was contracted to launch all the Iridium NEXT satellites. All the Iridium NEXT launches have taken place using a Falcon 9 rocket launch from Vandenberg Air Force Base in California. Deployment of the constellation began in January 2017, with the launch of the first ten Iridium NEXT satellites. Most recently, on January 11, 2019, SpaceX launched an additional ten satellites, bringing the number of upgraded satellites in orbit to 75.
In January 2020, the Iridium constellation was certified for use in the Global Maritime Distress and Safety System (GMDSS). The certification ended a monopoly on the provision of maritime distress services that had previously been held by Inmarsat since the system became operational in 1999.
The satellites each contained seven Motorola/Freescale PowerPC 603E processors running at roughly 200 MHz, connected by a custom backplane network. One processor was dedicated to each cross-link antenna ("HVARC"), and two processors ("SVARC"s) are dedicated to satellite control, one being a spare. Late in the project an extra processor ("SAC") was added to perform resource management and phone call processing.
The cellular look down antenna had 48 spot beams arranged as 16 beams in three sectors. The four inter-satellite cross links on each satellite operated at 10 Mbit/s. Optical links could have supported a much greater bandwidth and a more aggressive growth path, but microwave cross links were chosen because their bandwidth was more than sufficient for the desired system. 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. Iridium Satellite LLC stated that their second generation satellites would also use microwave, not optical, inter-satellite communications links. Iridium's cross-links are unique in the satellite telephone industry as other providers do not relay data between satellites; Globalstar and Inmarsat both use a transponder without cross-links.
The original design as envisioned in the 1960s was that of a completely static "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. 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. Moreover, fixed, static scheduling would have left more than 90% of the satellite links idle at all times. Therefore, the design was scrapped in favour 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 at 2400 bit/s and weighs about 680 kg (1,500 lb). The Iridium System presently operates within a 1618.85 to 1626.5 MHz band, part of the wider L-band, adjacent to the 1610.6-1613.8 MHz Radio Astronomy Service (RAS) band.
The configuration of the Satellite concept was designated as Triangular Fixed, 80 Inch Main Mission Antenna, Light-weight (TF80L). The packaging design of the spacecraft was managed by Lockheed Bus Spacecraft team; it was the first commercial satellite bus designed at the Sunnyvale Space Systems Division in California. The TF80L configuration was considered a non-conventional, innovative approach to developing a satellite design that could be assembled and tested in five days. The TF80L design configuration was also instrumental in simultaneously solving fundamental design problems involving optimization of the communications payload thermal environment and RF main mission antenna performance, while achieving the highest payload fairing packaging for each of the three main launch vehicle providers.
The first spacecraft mock-up of this design was built in the garage workshop in Santa Clara, California for the Bus PDR/CDR as a proof-of-concept model. This first prototype paved the way for the design and construction of the first engineering models. This design was the basis of the largest constellation of satellites deployed in low earth orbit . After ten years of successful on-orbit performance, the Iridium team celebrated the equivalent of 1,000 cumulative years of on-orbit performance in 2008. One of the engineering Iridium satellite models was placed on permanent exhibit in the Smithsonian Air and Space Museum in Washington DC.
95 of the 99 built satellites were launched between 1997 and 2002.[clarification needed] Three satellites were kept on the ground as spares.
The 95 satellites were launched over twenty-two missions (nine missions in 1997, ten in 1998, one in 1999 and two in 2002). One extra mission on Chang Zheng was a payload test and did not carry any actual satellites.
|Launch date||Launch site||Launch vehicle||Satellite number (at launch)|
|1997-05-05||Vandenberg||Delta II 7920-10C||4, 5, 6, 7, 8|
|1997-06-18||Baikonur||Proton-K/17S40||9, 10, 11, 12, 13, 14, 16|
|1997-07-09||Vandenberg||Delta II 7920-10C||15, 17, 18, 20, 21|
|1997-08-21||Vandenberg||Delta II 7920-10C||22, 23, 24, 25, 26|
|1997-09-01||Taiyuan||Chang Zheng 2C-III/SD||Iridium payload test / no satellite|
|1997-09-14||Baikonur||Proton-K/17S40||27, 28, 29, 30, 31, 32, 33|
|1997-09-27||Vandenberg||Delta II 7920-10C||19, 34, 35, 36, 37|
|1997-11-09||Vandenberg||Delta II 7920-10C||38, 39, 40, 41, 43|
|1997-12-08||Taiyuan||Chang Zheng 2C-III/SD||42, 44|
|1997-12-20||Vandenberg||Delta II 7920-10C||45, 46, 47, 48, 49|
|1998-02-18||Vandenberg||Delta II 7920-10C||50, 52, 53, 54, 56|
|1998-03-25||Taiyuan||Chang Zheng 2C-III/SD||51, 61|
|1998-03-30||Vandenberg||Delta II 7920-10C||55, 57, 58, 59, 60|
|1998-04-07||Baikonur||Proton-K/17S40||62, 63, 64, 65, 66, 67, 68|
|1998-05-02||Taiyuan||Chang Zheng 2C-III/SD||69, 71|
|1998-05-17||Vandenberg||Delta II 7920-10C||70, 72, 73, 74, 75|
|1998-08-19||Taiyuan||Chang Zheng 2C-III/SD||3, 76|
|1998-09-08||Vandenberg||Delta II 7920-10C||77, 79, 80, 81, 82|
|1998-11-06||Vandenberg||Delta II 7920-10C||2, 83, 84, 85, 86|
|1998-12-19||Taiyuan||Chang Zheng 2C-III/SD||11a, 20a|
|1999-06-11||Taiyuan||Chang Zheng 2C-III/SD||14a, 21a|
|2002-02-11||Vandenberg||Delta II 7920-10C||90, 91, 94, 95, 96|
^ Iridium satellite number changed over time following failure and replacement.
Spare satellites are usually held in a 666 km (414 mi) storage orbit. These can be boosted to the correct altitude and put into service in case of a satellite failure. After the Iridium company emerged from bankruptcy the new owners decided to launch seven new spares, which would have ensured two spare satellites were available in each plane. As of 2009 , not every plane had a spare satellite; however, the satellites can be moved to a different plane if required. A move can take several weeks and consumes fuel which will shorten the satellite's expected service life.
Significant orbital inclination changes are normally very fuel-intensive, but orbital perturbation analysis aids the process. 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. The Iridium satellites have an inclination of 86.4°, which places every satellite in a prograde (inclination < 90°) orbit. This causes their equator crossings to 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. 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. Although this saves substantial amounts of fuel, it can be a time-consuming process.
As of mid-2016, Iridium has experienced in-orbit failures which cannot be corrected with in-orbit spare satellites, thus only 64 of the 66 satellites required for seamless global coverage were in operation. Therefore, service interruptions can be observed, especially around the equatorial region where the satellite footprints are most spread out and there is least overlap.
In 2017, Iridium began launching Iridium NEXT, a second-generation worldwide network of telecommunications satellites, consisting of 66 active satellites, with another nine in-orbit spares and six on-ground spares. These satellites incorporate features such as data transmission that were not emphasized in the original design. The constellation provides L-band data speeds of up to 128 kbit/s to mobile terminals, up to 1.5 Mbit/s to Iridium Pilot marine terminals, and high-speed Ka-band service of up to 8 Mbit/s to fixed/transportable terminals. The next-generation terminals and service became commercially available in 2018.
The NEXT satellites incorporate a secondary payload for Aireon, a space-qualified ADS-B data receiver for use by air traffic control and, via FlightAware, by airlines. A tertiary payload on 58 satellites is a marine AIS ship-tracker receiver for Canadian company exactEarth Ltd.
Iridium NEXT also provides data link to other satellites in space, enabling command and control of other space assets regardless of the position of ground stations and gateways.
In June 2010, Iridium signed the largest commercial rocket-launch deal ever at that time, a US$492 million contract with SpaceX to launch 70 Iridium NEXT satellites on seven Falcon 9 rockets from 2015 to 2017 via SpaceX leased launch facility at Vandenberg Air Force Base. The final two satellites were originally slated to be orbited by a single launch of an ISC Kosmotras Dnepr. Technical issues and consequential demands from Iridium's insurance delayed the launch of the first pair of Iridium NEXT satellites until April 2016.
Iridium NEXT launch plans originally included launch of satellites on both Ukrainian Dnepr launch vehicles and SpaceX Falcon 9 launch vehicles, with the initial satellites launching on Dnepr in April 2016; however, in February 2016, Iridium announced a change. Due to an extended slowdown in obtaining the requisite launch licenses from Russian authorities, Iridium revamped the entire launch sequence for the 75-satellite constellation. It launched and successfully deployed 10 satellites with SpaceX on January 14, 2017, delayed due to weather from January 9, 2017, and the first of those new satellites took over the duties of an old satellite on March 11, 2017.
At the time of the launch of the first batch, the second flight of ten satellites was planned to launch only three months later in April 2017. However, in a February 15 statement, Iridium said that SpaceX pushed back the launch of its second batch of Iridium NEXT satellites from mid-April to mid-June 2017. This second launch, which occurred on June 25, 2017, delivered another ten Iridium NEXT satellites to low Earth-orbit (LEO) on a SpaceX Falcon 9 rocket. A third launch, which occurred on October 9, 2017, delivered another ten satellites to LEO, as planned. The Iridium NEXT IV mission launched with ten satellites on December 23, 2017. The fifth mission, Iridium NEXT V, launched with ten satellites on March 30, 2018. The sixth launch on May 22, 2018, sent another 5 satellites into LEO. The penultimate Iridium NEXT launch occurred on July 25, 2018 launching another 10 Iridium NEXT satellites. The final ten NEXT satellites launched on January 11, 2019. Six additional satellites are in storage on the ground as spares.
|Launch date||Launch site||Launch vehicle||Satellite numbers (at launch)|
|2017-01-14||Vandenberg||Falcon 9 FT||102, 103, 104, 105, 106, 108, 109, 111, 112, 114|
|2017-06-25||Vandenberg||Falcon 9 FT||113, 115, 117, 118, 120, 121, 123, 124, 126, 128|
|2017-10-09||Vandenberg||Falcon 9 B4||100, 107, 119, 122, 125, 129, 132, 133, 136, 139|
|2017-12-23||Vandenberg||Falcon 9 FT||116, 130, 131, 134, 135, 137, 138, 141, 151, 153|
|2018-03-30||Vandenberg||Falcon 9 B4||140, 142, 143, 144, 145, 146, 148, 149, 150, 157|
|2018-05-22||Vandenberg||Falcon 9 B4||110, 147, 152, 161, 162|
|2018-07-25||Vandenberg||Falcon 9 B5||154, 155, 156, 158, 159, 160, 163, 164, 165, 166|
|2019-01-11||Vandenberg||Falcon 9 B5||167, 168, 169, 170, 171, 172, 173, 175, 176, 180|
^ Iridium satellite number could change over time following failure and replacement.
The main patents on the Iridium system, U.S. Patents 5,410,728: "Satellite cellular telephone and data communication system", and 5,604,920, are in the field of satellite communications, and the manufacturer generated several hundred patents protecting the technology in the system. Satellite manufacturing initiatives were also instrumental in the technical success of the system. Motorola made a key hire of the engineer who set up the automated factory for Apple's Macintosh. 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. At its peak during the launch campaign in 1997 and 1998, Motorola produced a new satellite every 4.3 days, with the lead-time of a single satellite being 21 days.[non-primary source needed]
Over the years a number of Iridium satellites have ceased to work and are no longer in active service, some are partially functional and have remained in orbit whereas others have tumbled out of control or have reentered the atmosphere.
Iridium 21, 27, 20, 11, 24, 71, 44, 14, 79, 69 and 85 all suffered from issues before entering operational service soon after their launch in 1997. By 2018, of these eleven, Iridium 21, 27, 79 and 85 have decayed out of orbit; Iridium 11, 14, 20 and 21 were renamed to Iridium 911, 914, 920 and 921 respectively since replacements of the same name were launched.
From 2017, several first-generation Iridium satellites have been deliberately de-orbited after being replaced by operational Iridium NEXT satellites.
|List of defunct Iridium satellites previously in operating service|
|Iridium 2||?||?||Uncontrolled orbit|
|Iridium 73||~1998||Iridium 75||Uncontrolled orbit|
|Iridium 48||May 2001||Iridium 20||Decayed May 2001|
|Iridium 9||October 2000||Iridium 84||Decayed March 2003|
|Iridium 38||September 2003||Iridium 82||Uncontrolled orbit|
|Iridium 16||April 2005||Iridium 86||Uncontrolled orbit|
|Iridium 17||August 2005||Iridium 77||Uncontrolled orbit|
|Iridium 74||January 2006||Iridium 21||In orbit as spare|
|Iridium 36||January 2007||Iridium 97||Uncontrolled orbit|
|Iridium 28||July 2008||Iridium 95||In orbit|
|Iridium 33||February 2009||Iridium 91||Destroyed February 2009|
(Collided with Kosmos 2251)
|Iridium 26||August 2011||Iridium 11||In orbit|
|Iridium 7||July 2012||Previously Iridium 51*||Failed in orbit|
|Iridium 4||2012||Iridium 96||In orbit|
|Iridium 29||Early 2014||Iridium 45||In orbit|
|Iridium 42||August 2014||Iridium 98||Uncontrolled orbit|
|Iridium 63||August 2014||Iridium 14||In orbit|
|Iridium 6||October 2014||*Iridium 51||Decayed 23 December 2017|
|Iridium 57||May 2016||Iridium 121||Observed drifting from nominal position|
|Iridium 39||June 2016||Iridium 15||In orbit|
|Iridium 74||June 2017||(spare)||Decayed June 2017|
|Iridium 30||August 2017||Iridium 126||Decayed September 2017|
|Iridium 77||August 2017||Iridium 109||Decayed September 2017|
|Iridium 8||November 2017||Iridium 133||Decayed 24 November 2017|
|Iridium 34||December 2017||Iridium 122||Decayed 8 January 2018|
|Iridium 43||Decayed 11 February 2018||Iridium 111||Decaying orbit|
|Iridium 3||Decayed 8 February 2018||Iridium 131||Decaying orbit|
|Iridium 21||Decayed 24 May 2018||Decayed|
|Iridium 37||Decayed 26 May 2018||Decayed|
|Iridium 68||Decayed 6 June 2018||Decayed|
|Iridium 67||Decayed 2 July 2018||Decayed|
|Iridium 75||Decayed 10 July 2018||Decayed|
|Iridium 81||Decayed 17 July 2018||Decayed|
|Iridium 65||Decayed 19 July 2018||Decayed|
|Iridium 41||Decayed 28 July 2018||Decayed|
|Iridium 80||Decayed 12 August 2018||Decayed|
|Iridium 18||Decayed 19 August 2018||Decayed|
|Iridium 66||Decayed 23 August 2018||Decayed|
|Iridium 98||Decayed 24 August 2018||Decayed|
|Iridium 76||Decayed 28 August 2018||Decayed|
|Iridium 47||Decayed 1 September 2018||Decayed|
|Iridium 12||Decayed 2 September 2018||Decayed|
|Iridium 50||Decayed 23 September 2018||Decayed|
|Iridium 40||Decayed 23 September 2018||Decayed|
|Iridium 53||Decayed 30 September 2018||Decayed|
|Iridium 86||Decayed 5 October 2018||Decayed|
|Iridium 10||Decayed 6 October 2018||Decayed|
|Iridium 70||Decayed 11 October 2018||Decayed|
|Iridium 56||Decayed 11 October 2018||Decayed|
|Iridium 15||Decayed 14 October 2018 (Over No. Pacific)||Decayed|
|Iridium 20||Decayed 22 October 2018||Decayed|
|Iridium 11||Decayed 22 October 2018||Decayed|
|Iridium 84||Decayed 4 November 2018||Decayed|
|Iridium 83||Decayed 5 November 2018||Decayed|
|Iridium 52||Decayed 5 November 2018||Decayed|
|Iridium 62||Decayed 7 November 2018||Decayed|
|Iridium 31||Decayed 20 December 2018||Decayed|
|Iridium 35||Decayed 26 December 2018||Decayed|
|Iridium 90||Decayed 23 January 2019||Decayed|
|Iridium 32||Decayed 10 March 2019||Decayed|
|Iridium 59||Decayed 11 March 2019||Decayed|
|Iridium 91||Decayed 13 March 2019||Decayed|
|Iridium 14||Decayed 15 March 2019||Decayed|
|Iridium 60||Decayed 17 March 2019||Decayed|
|Iridium 95||Decayed 25 March 2019||Decayed|
|Iridium 55||Decayed 31 March 2019||Decayed|
|Iridium 64||Decayed 1 April 2019||Decayed|
|Iridium 58||Decayed 7 April 2019||Decayed|
|Iridium 54||Decayed 11 May 2019||Decayed|
|Iridium 24||Decayed 12 May 2019||Decayed|
|Iridium 61||Decayed 23 July 2019||Decayed|
|Iridium 97||Decayed 27 December 2019||Decayed|
At 16:56 UTC on February 10, 2009, Iridium 33 collided with the defunct Russian satellite Kosmos 2251. This accidental collision was the first hypervelocity collision between two artificial satellites in low Earth orbit. Iridium 33 was in active service when the accident took place. It was one of the oldest satellites in the constellation, having been launched in 1997. The satellites collided at a relative speed of roughly 35,000 km/h (22,000 miles per hour) This collision created large amounts of space debris that can be hazardous to other satellites.[clarification needed]
Iridium moved one of its in-orbit spares, Iridium 91 (formerly known as Iridium 90), to replace the destroyed satellite, completing the move on March 4, 2009.
Communication between satellites and handsets is done using a TDMA and FDMA based system using L-band spectrum between 1616 and 1626.5 MHz. Iridium exclusively controls 7.775 MHz of this and shares a further 0.95 MHz. In 1999 Iridium agreed to timeshare a portion of spectrum, allowing radio astronomers to observe hydroxyl emissions; the amount of shared spectrum was recently reduced from 2.625 MHz.
External "hockey puck" type antennas used with Iridium handheld phones, data modems and SBD terminals are usually defined as 3dBi gain, 50 ohm impedance with RHCP (right hand circular polarization) and 1.5:1 VSWR. As Iridium antennas function in frequencies very close to that of GPS, a single antenna may be utilized through a pass-through for both Iridium and GPS reception.
The type of modulation used is normally DE-QPSK, although DE-BPSK is used on the uplink (mobile to satellite) for acquisition and synchronization. Each time slot is 8.28 ms long and sits in a 90 ms frame. Within each FDMA channel there are four TDMA time slots in each direction. The TDMA frame starts off with a 20.32 ms period used for simplex messaging to devices such as pagers and to alert Iridium phones of an incoming call, followed by the four upstream slots and four downstream slots. This technique is known as time-division multiplexing. Small guard periods are used between time slots. Regardless of the modulation method being used, communication between mobile units and satellites is performed at 25 kilobaud.
Channels are spaced at 41.666 kHz and each channel occupies a bandwidth of 31.5 kHz; this allows space for Doppler shifts.
The Iridium system uses three different handoff types. As a satellite travels over the horizon, calls are handed to adjacent spot-beams; this occurs approximately every fifty seconds. A satellite only stays in view for seven minutes at the equator. When the satellite disappears from view, an attempt is made to hand the call to another satellite. If no other satellite is in view, the connection is dropped. This may occur when the signal from either satellite is blocked by an obstacle. When successful, the inter-satellite handoff may be noticeable by a quarter-second interruption.
The satellites are also able to transfer mobile units to different channels and time slots within the same spot beam.
Iridium routes phone calls through space. In addition to communicating with the satellite phones in its footprint, each satellite in the constellation also maintains contact with two to four adjacent satellites, and routes data between them, to effectively create a large mesh network. There are several earth stations which link to the network through the satellites visible to them. The space-based backhaul routes outgoing phone call packets through space to one of the earth station downlinks ("feeder links"). Station-to-station calls from one satellite phone to another can be routed directly through space without going through an earth station. As satellites leave the area of an earth station, the routing tables are updated and packets headed for the earth station are forwarded to the next satellite just coming into view of the earth station. Communication between satellites and earth stations is at 20 and 30 GHz.
Gateways are located in
The pre-bankruptcy corporate incarnation of Iridium built eleven gateways, most of which have since been closed.