Mission Specification


The Cyclone Global Navigation Satellite System (CYGNSS) is a NASA Earth System Science Pathfinder Mission that will collect the first frequent space‐based measurements of surface wind speeds in the inner core of tropical cyclones. Made up of a constellation of eight microsatellites, the observatories will provide nearly gap-free Earth coverage using an orbital inclination of approximately 35° from the equator, with a mean (i.e., average) revisit time of seven hours and a median revisit time of three hours. This inclination will allow CYGNSS to measure ocean surface winds between 38° N and 38° S latitude. This range includes the critical latitude band for tropical cyclone formation and movement.

CYGNSS will measure the ocean surface wind field with unprecedented temporal resolution and spatial coverage, under all precipitating conditions, and over the full dynamic range of wind speeds experienced in a tropical cyclone. The mission will accomplish this through an innovative combination of all-weather performance Global Positioning System (GPS) reflectometry with the sampling properties of a dense constellation of eight observatories.

What makes CYGNSS unique is that it will be NASA’s first mission to perform surface remote sensing using an existing Global Navigation Satellite System (GNSS)— a satellite constellation that is used to pinpoint the geographic location of a user’s receiver anywhere in the world. A number of GNSS systems are currently in operation, including: the United States’ Global Positioning System (GPS), the European Galileo, the Russian Federation’s Global Orbiting Navigation Satellite System (GLONASS), and the Chinese Beidou. CYGNSS will use the United States’ GPS constellation.

Unlike radar scatterometers (e.g., ISS-RapidScat, QuikSCAT, and ASCAT) that both emit microwave radar pulses and receive their backscattered signals, CYGNSS is functions as a constellation of passive sensors that receive the signal of surface-reflected GPS pulses. One of the most well-known limitations of traditional microwave scatterometry (particularly, Ku-band) is signal degradation of the microwave pulses when passing through intense rainfall as typically observed within hurricane eyewalls, thus limiting its utility in retrieving observations of high wind speeds in this critical region of the storm. Reflected GPS signals, on the other hand, operate at a much lower microwave frequency utilized by the GPS constellation that is able to penetrate thick clouds and precipitation around the eyewall and provide the first opportunity to remotely measure inner-core wind speeds.

The goal of the mission is to study the relationship between ocean surface properties (i.e., surface wind speed), moist atmospheric thermodynamics, heat transfer, and convective dynamics in the inner core of a tropical cyclone. This will allow scientists to determine how a tropical cyclone forms, whether or not it will strengthen, and if so by how much. The successful completion of these goals will allow the mission to contribute to the advancement of tropical cyclone forecasting and tracking methods.

Platform/Instrument Specification
  • Launch Date: 15 December 2016
  • 8 Observatory Platforms
  • Mass (each): 27.5 kg
  • Spacecraft Altitude: 510 km
  • Orbit Inclination: 35°
  • Orbit Period: 95 minutes