The initial Sensor Network consists of a number of spacecraft in low-earth orbit equipped with a GPS Radio Occultation sensor. This sensor, a modified GPS receiver, measures properties of the received signal and from it determines properties of the atmosphere. GPS Radio Occultation (GPS-RO) provides measurements of refractivity, and with it temperature and pressure, of the the atmosphere. Over time additional sensor types will be added to the network to expand measurement types and frequency.

The GPS Radio Occultation derived data is among the worlds most accurate measurement of temperature – done on a global scale, in real time. This data is actively being used for operational weather forecasting and climate monitoring.


The arrival of the Global Positioning System (GPS) in the 1980s made the idea both practical and (potentially) useful for the first time. GPS-RO is possible because the GPS system designers in the early 1970s had the vision to extend the transmission beamwidths comfortably beyond the Earth’s limb. All we need now is a suitably programmed GPS receiver on a low Earth satellite, pointed at the Earth’s limb.

Schematic view of the GPS occultation process.

The rapid motion of the low orbiting receiver dominates the changing geometry and largely determines the duration of the occultation — typically about one minute. The much higher GPS satellites move relatively slowly and can be regarded as almost stationary during the occultation. For that reason, most occultations occur in the forward or backward direction with respect to the receiver’s line of motion, with relatively few occurring off to the sides.


We can think of the transmitted GPS signals as sinusoidal electromagnetic waves. Each satellite broadcasts at two radio frequencies, about 1.2 and 1.6 billion cycles per second (gigahertz).  Traveling at the speed of light, these signals have wavelengths of about 24 and 19 cm, or roughly 4 and 5 wavelengths per meter, respectively.  Thus over a distance of 100 m, the two signals complete a little more than 400 and 500 cycles.  In principle one can measure distance by counting the number of cycles between a transmitter and a receiver. As an orbiting receiver watches a GPS signal set (or rise from) behind the earth, the signal must pass through the atmosphere in a limb-grazing geometry.  The atmosphere bends and delays the signal, increasing its effective path length and thus the number of cycles along the raypath. At the surface the increased path length caused by the atmosphere can reach 2.5 km — or more than 12,000 cycles at the shorter wavelength. By counting the extra cycles we can measure this “excess delay” with a precision of about 0.005 cycle, or ~1 mm — better than one part in a million. This accounts for the extraordinary performance of GPS-RO in recovering atmospheric profiles.

From these profiles we can compute climate averages, contour maps, and wind fields — and watch the atmosphere expand as it warms. We note that in the lowest few km where moisture can become prominent the contributions of temperature and moisture to the signal delay become ambiguous. However, since we can model (project downward from ~5 km altitude) the temperature based on climatological patterns, we can then recover moisture in the lower atmosphere with high accuracy. Actual weather models generally don’t bother with this. They simply ingest the pure refractivity or bending angle measurement, which is not ambiguous, and let the detailed physics built into the model, combined with information from other sensors, sort out the relative contributions of temperature and moisture at different altitudes, a strategy that has proven highly effective.


Here is one of the first GPS-RO temperature profiles ever recorded, acquired by GPS/MET on April 5, 1995 — just one day after launch. The RO profile is compared against a nearby weather balloon (radiosonde) profile and a weather model estimate from the European Center for Medium-range Weather Forecasts (ECMWF). Note that the model profile cannot capture the detail of the other two.  (GPS retrieval by JPL, 1995)

The red dots are the locations of the world’s weather balloon launch sites. Each site lofts a balloon every 12 hours at 0:00 and 12:00 universal time. The green dots show the 1-day GPS-RO coverage with six COSMIC satellites.  (Illustration by COSMIC Project, UCAR)

3D electron density model

Electron density profiles can be combined tomographically to generate accurate 3D maps of the global electron distribution updated every few minutes. This can be invaluable in monitoring and eventually predicting hazardous geomagnetic storms caused by solar activity. (Fig. from Mannucci et al., 2nd GPSRO Users Workshop, Aug 2005.)








  1. High accuracy: Averaged profiles to <0.1K
  2. Assured long-term stability
  3. All-weather, day-night operation
  4. Global 3D coverage: stratopause to surface
  5. High vertical resolution: ~100m in lower trop
  6. Independent height & pressure/temp data
  7. Compact, low-power, low-cost sensor



Mariner IV approaching Mars July 15, 1965

July 15, 1965. Mariner IV was transmitting data as it was coming in for the closest approach around Mars. In the moments as it disappeared behind the planet, the transmitted signal, as viewed from Earth, passed through the thin Martian atmosphere, from its upper reaches down to the surface, executing history’s first planetary atmospheric and ionospheric radio occultation experiments. Minutes later as the signal reappeared on the other side of the planet, the first rising occultation was observed from Earth.

Subsequent occultation experiments were performed at Venus,and the outer planets, Jupiter and Saturn Uranus and Neptune, and many of their moons. In fact most major bodies of the solar system were studied by radio occultation before we began to look homeward. For radio occultation to be of use in studying the environs of Earth, which we can observe at close hand by other means, we need many signal sources in space — a tall order.


Radio Occultation Satellites 1998-2005

The first proof-of-concept experiment, called GPS/MET (for GPS Meteorological experiment) was launched in April 1995 and was a breakthrough success for the GPS-RO technique. NASA followed by sponsoring five JPL-led GPS-RO experiments on five different international missions from 1998-2005. These missions included Ørsted (Danish), Sunsat (South African), CHAMP (German), SAC-C (Argentine), and GRACE (US-German).

In April 2006, the pioneering six-satellite COSMIC (Constellation Observing System for Meteorology, Ionosphere, and Climate) mission, sponsored primarily by Taiwan’s National Space Organization and managed in the U.S. by UCAR, was launched on a Minotaur rocket from Vandenberg AFB, becoming the first dedicated constellation for demonstrating the operational use of GPS-RO data in weather forecasting. COSMIC is expected to operate until about 2011.


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