21.7 Low Earth Orbit Systems: Iridium & COSPAS-SARSAT

Key Takeaways

  • The Iridium satellite constellation orbits at an altitude of 485 miles and uses 1616-1626 MHz for telephone and messaging
  • Iridium provides digital voice and data at 2.4 kbps, with 48 spot beams per satellite and a footprint about 30 miles in diameter per beam
  • The main function of the COSPAS-SARSAT satellite system is to monitor 406 MHz for distress calls from EPIRBs
  • COSPAS-SARSAT determines the position of a ship in distress by measuring the Doppler shift of the 406 MHz signal at several different points in its orbit
  • Low earth orbit gives short path delay and polar coverage, which is why Iridium and COSPAS-SARSAT work where geostationary Inmarsat does not
Last updated: August 2026

21.7 Low Earth Orbit Systems: Iridium & COSPAS-SARSAT

Quick Answer: Iridium: orbit 485 miles, band 1616–1626 MHz, digital voice and data at 2.4 kbps, 48 spot beams per satellite with a 30-mile footprint each. COSPAS-SARSAT: monitors 406 MHz for distress calls from EPIRBs, and fixes position by measuring the Doppler shift of the 406 MHz signal at several different points in its orbit.

Sub-topic 3-P-095 (Low Earth Orbit Systems) covers the two LEO constellations a marine technician meets. It pairs naturally with the geostationary Inmarsat material, because the contrast between the two orbit types explains everything about what each system can do.

Why low earth orbit at all

Geostationary (Inmarsat)Low earth orbit (Iridium, COSPAS-SARSAT)
Altitude~22,300 miles~485 miles (Iridium)
CoverageNear-global except the polesIncluding the poles
Path delay~250 ms round tripTens of milliseconds
Terminal power / antennaHigher gain neededModest — a handset works
Satellites needed3–4Dozens

Two consequences drive everything else. First, a geostationary satellite sits above the equator, so from high latitudes it is at or below the horizon — which is exactly why sea area A4 (the polar regions) is defined as the area outside Inmarsat coverage, and why LEO systems matter there. Second, because a LEO satellite is roughly 46 times closer, path loss is dramatically lower and a handheld terminal becomes practical.

Iridium: the numbers

The pool asks four separate factual items about Iridium, so learn them as a block:

ParameterValue
Orbiting altitude485 miles
Frequency band (telephone and messaging)1616–1626 MHz
Services providedDigital voice and data at 2.4 kbps
Spot beams48 per satellite, footprint about 30 miles in diameter

A few notes that make the numbers stick:

  • 1616–1626 MHz is in L-band, the same general region as GPS (1227.6 and 1575.4 MHz, section 21.8) and Inmarsat. L-band is used for mobile satellite service because it penetrates weather with minimal rain fade and works with small, non-tracking antennas.
  • 2.4 kbps sounds slow, and it is — Iridium was designed around voice and short messaging, not broadband. For a GROL technician the relevance is that a vessel's Iridium terminal is for telephony, position reporting and short data, not for bulk transfer.
  • 48 spot beams per satellite is how the constellation reuses its limited spectrum: each satellite paints its coverage as a honeycomb of small beams, and the same frequencies serve non-adjacent beams simultaneously — the same cellular principle used on land, projected from orbit.
  • Because the satellites move fast relative to the ground, a call is handed off between beams and between satellites during a conversation, which is why the system needs inter-satellite links.

COSPAS-SARSAT

What is the main function of the COSPAS-SARSAT satellite system? Monitor 406 MHz for distress calls from EPIRBs.

COSPAS-SARSAT is the alerting backbone of GMDSS. It is an international, government-run, non-commercial system whose only job is to detect and locate distress beacons — EPIRBs at sea (section 5.2), ELTs in aircraft, and PLBs carried by individuals.

406 MHz is the frequency to remember. It is dedicated to satellite distress alerting, and a 406 MHz beacon transmits a digitally coded burst carrying a unique identity that ties back to a registration database — vessel name, owner, emergency contacts.

Position by Doppler shift

How does the COSPAS-SARSAT satellite system determine the position of a ship in distress? By measuring the Doppler shift of the 406 MHz signal taken at several different points in its orbit.

This is the elegant part, and worth understanding rather than memorising.

A LEO satellite passing overhead is moving fast relative to the beacon. As it approaches, the received frequency is shifted up; as it recedes, shifted down. The instant of zero Doppler shift — the moment the frequency crosses the beacon's true value — occurs at the satellite's closest approach. The rate at which the shift changes through that crossing indicates how close the pass was.

Take those measurements at several points along the orbital pass, combine them with the precisely known satellite ephemeris, and the beacon's position falls out — typically to within a few kilometres, with no position data required from the beacon at all.

Two practical points follow:

  1. Doppler location needs relative motion, so it works with LEO satellites, not geostationary ones. The geostationary part of COSPAS-SARSAT provides instant alerting but no Doppler position.
  2. A modern GPS-equipped EPIRB transmits its own position inside the 406 MHz message, giving a fix in minutes instead of the up-to-an-hour wait for a suitable satellite pass. Doppler remains the fallback and remains the pool's answer.

Recall from section 5.2 that COSPAS-SARSAT is the international satellite-based SAR system that detects and locates 406 MHz EPIRB alerts — the same fact framed from the Element 1 side.

Test Your Knowledge

What is the orbiting altitude of the Iridium satellite communications system, and what frequency band does it use for telephone and messaging?

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Test Your Knowledge

What is the main function of COSPAS-SARSAT, and how does it determine the position of a ship in distress?

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Test Your Knowledge

What services does the Iridium system provide, and how is its spectrum reused?

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Test Your Knowledge

Why does GMDSS rely on low earth orbit satellites for polar regions rather than geostationary Inmarsat?

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