GPS BIIF-1 (PRN 25)

NORAD 36585· COSPAR 2010-022A· Navigation· MEO
Launch
Launched on May 28, 2010 from Space Launch Complex 37B, United States of America aboard a Delta IV M+(4,2).
Delta IV M+(4,2) | GPS IIF SV-1 (USA-213)
GPS BIIF-1  (PRN 25)
USAF · Public domain · via Wikimedia Commons
Live · TLE epoch 2026-07-13 10:43 UTC
Orbit class
MEO — Medium Earth (2,000–30,000 km, e.g. GPS / Galileo)
Operator
United States Air Force
Country
United States
Manufacturer
Boeing
Launched
May 28, 2010
Mass
Apogee
20,526 km
Perigee
19,853 km
Inclination
54.27°
Period
11.97 h

About GPS BIIF-1 (PRN 25)

GPS BIIF-1, cataloged by NORAD as object 36585 and carrying the international designator 2010-022A, is the first satellite of the Block IIF generation of the United States Air Force's Global Positioning System constellation. Better known by its operational designations USA-213 and PRN 25, it was lofted into medium Earth orbit on 27 May 2010 (28 May 2010 UTC) and remains operational to this day. As the pathfinder for an upgraded GPS lineage, it occupies a historically significant place in the decades-long evolution of the world's most widely used satellite navigation system.

Mission and Purpose

The Global Positioning System is a constellation of navigation satellites maintained by the United States Air Force that provides continuous, all-weather positioning, navigation, and timing (PNT) services to military and civilian users worldwide. Each satellite in the constellation continuously broadcasts ranging signals on multiple radio frequencies; receivers on the ground — or aboard ships, aircraft, or other spacecraft — compute their position by measuring the time it takes for those signals to arrive from multiple satellites simultaneously.

GPS BIIF-1 transmits on the PRN 25 slot within the constellation. A pseudorandom noise (PRN) code is a unique identifier that allows a receiver to distinguish one GPS satellite's signal from another, and each operational satellite is assigned a specific PRN channel. The PRN 25 assignment previously belonged to an older Block II satellite, USA-79, which had provided that signal for nearly eighteen years before being retired in late 2009. GPS BIIF-1 stepped into that role, carrying forward the PRN 25 signal with the enhanced capabilities of a newer generation of hardware.

The Block IIF series represented a meaningful advancement over earlier GPS generations. IIF satellites were designed to carry a third civilian frequency signal — the L5 signal — in addition to the legacy L1 and L2 signals. L5, operating in a frequency band protected for aeronautical safety-of-life services, is intended to improve accuracy and reliability for aviation, emergency services, and other safety-critical applications. By being the first IIF satellite on orbit, GPS BIIF-1 validated the design and initiated operational use of these expanded capabilities within the live constellation.

The satellite was assigned to Plane B of the GPS constellation. The GPS constellation is organized into six orbital planes, each containing multiple satellites spaced to ensure that at least four satellites are visible from virtually any point on Earth's surface at any given time. Placement in Plane B was chosen to fill or reinforce coverage in that region of the constellation, maintaining the global continuity of PNT service.

The mission's operator is the United States Air Force, which has managed the GPS program since its origins in the 1970s. Day-to-day operations — including uploading navigation data, monitoring satellite health, and managing the constellation — are handled by the 2nd Space Operations Squadron (2 SOPS) at Schriever Air Force Base in Colorado.

Orbit and Tracking

GPS BIIF-1 resides in medium Earth orbit (MEO), the orbital regime that has been home to GPS satellites since the program's inception. Its current tracked orbital parameters place it at an apogee of approximately 20,525 km and a perigee of approximately 19,854 km above Earth's surface. The relatively small difference between these two figures indicates a nearly circular orbit, which is characteristic of navigation satellites — a circular orbit ensures that the satellite's altitude, and therefore the geometry of its ranging signals, remains consistent over the course of each pass.

The satellite's orbital inclination is 54.3°, meaning its orbital plane is tilted 54.3 degrees relative to Earth's equatorial plane. This inclination, shared across the GPS constellation, allows the satellites to provide coverage at all latitudes up to and including the polar regions, though coverage geometry is somewhat better at mid-latitudes where the bulk of global navigation demand is concentrated.

The orbital period is approximately 718.0 minutes, or just under twelve hours. This is the hallmark of the GPS orbital regime: a roughly half-sidereal-day period causes each satellite to trace the same ground track twice per sidereal day, making the constellation's coverage pattern highly predictable and geometrically stable over time. Ground control stations can therefore anticipate satellite positions with great precision, which is essential for uploading accurate navigation message data.

NORAD tracks GPS BIIF-1 under catalog number 36585. As with all tracked objects in Earth orbit, its position is continually refined through ground-based radar and optical observations, and updated two-line element (TLE) sets are regularly published. The satellite has shown no signs of decay and remains in its designed operational orbit.

Design and Operator

GPS BIIF-1 was designed and built by Boeing under contract to the United States Air Force. Boeing's Space and Defense division was selected to manufacture the Block IIF series, which ultimately comprised twelve satellites. The IIF designation stands for "Block II Follow-on," reflecting the satellite's role as a continuation and improvement of the long-running GPS Block II production lineage rather than a wholly new design philosophy.

Block IIF satellites were built with a design life intended to exceed the operational lifetimes of earlier GPS generations, incorporating upgrades to onboard atomic clocks — the most critical components for timing accuracy — as well as improved signal generation electronics and enhanced resistance to jamming and spoofing. The satellites also carry rubidium and cesium atomic frequency standards to provide the extraordinarily stable timing references upon which GPS navigation mathematics depend.

The satellite's mass is not publicly recorded in standard orbital catalogs. Its launch vehicle was a United Launch Alliance Delta IV Medium+(4,2) rocket, which lifted off from Space Launch Complex 37B at Cape Canaveral Air Force Station in Florida. The Delta IV family was a workhorse of U.S. government space launches during this era, and the Medium+(4,2) configuration — featuring a central common booster core augmented by two solid rocket motors and a four-meter payload fairing — was well matched to the mass and orbit requirements of GPS IIF payloads.

As a United States government asset, GPS BIIF-1 is owned and operated by the United States, with the Air Force bearing operational responsibility. Following the 2019 establishment of the United States Space Force, GPS constellation management has transitioned to that newer branch of the armed services, though the satellite itself predates that organizational change.

Significance and Legacy

The launch of GPS BIIF-1 on 27 May 2010 opened a new chapter in GPS modernization. As the first satellite of its series to reach orbit, it carried the weight of proving out new hardware and new signal capabilities in the demanding environment of medium Earth orbit. A single technical failure on a first-of-type satellite can delay an entire production run; GPS BIIF-1's successful deployment and commissioning cleared the path for the eleven subsequent Block IIF satellites that followed between 2011 and 2016.

The introduction of the L5 signal via the IIF series has had lasting consequences for GPS receiver technology. Modern high-precision receivers — used in surveying, precision agriculture, autonomous vehicles, and aviation — routinely exploit multi-frequency signals to model and remove ionospheric delay errors, which had long been one of the dominant sources of GPS ranging error. GPS BIIF-1 was among the first operational satellites to make that capability available on the live constellation.

The PRN 25 signal it broadcasts has been in continuous use for decades, carried first by older satellites and now sustained by GPS BIIF-1. From a user's perspective, the continuity of the PRN 25 slot across satellite generations is seamless — receivers do not distinguish between which physical satellite is broadcasting a given PRN, only that the signal is present and healthy. This architectural flexibility has allowed the Air Force to modernize the constellation incrementally without disrupting the billions of devices that depend on it.

As of the date of this article, GPS BIIF-1 remains in orbit and continues to contribute to global navigation services. The Block IIF series as a whole has been succeeded in production by the Block III generation, built by Lockheed Martin, which began launching in 2018. However, IIF satellites including GPS BIIF-1 are expected to remain in service until they are retired and replaced by Block III vehicles as the constellation is progressively refreshed. The satellite's longevity is itself a testament to the design margins built into the IIF platform by Boeing and its Air Force partners. Barring unforeseen anomalies, GPS BIIF-1 will continue to silently broadcast its timing pulses from roughly 20,000 kilometers overhead for years to come.

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