GPS BIIF-6 (PRN 06)

NORAD 39741· COSPAR 2014-026A· Navigation· MEO
Launch
Launched on May 17, 2014 from Space Launch Complex 37B, United States of America aboard a Delta IV M+(4,2).
Delta IV M+(4,2) | GPS IIF-6 (USA-251)
GPS BIIF-6  (PRN 06)
via Wikimedia Commons
Live · TLE epoch 2026-07-13 09:17 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 17, 2014
Mass
Apogee
20,291 km
Perigee
20,088 km
Inclination
56.48°
Period
11.97 h

About GPS BIIF-6 (PRN 06)

GPS BIIF-6, catalogued by NORAD under identifier 39741 and carrying the international designator 2014-026A, is an American navigation satellite operating as part of the Global Positioning System constellation. Launched in May 2014, it is more formally designated GPS IIF-6 and carries the satellite vehicle number SVN-67, also known as NAVSTAR 70. The spacecraft represents the sixth of twelve satellites in the Block IIF series to reach orbit, and as of the time of writing it remains operational in medium Earth orbit, contributing to the continuous provision of positioning, navigation, and timing services relied upon by military and civilian users worldwide.

Mission and Purpose

The Global Positioning System is a satellite-based navigation infrastructure maintained by the United States government and operated by the United States Air Force. At its core, GPS functions by having a constellation of satellites transmit precisely timed radio signals; receivers on the ground, at sea, or in the air calculate their position by measuring the time it takes for signals to arrive from multiple satellites simultaneously. For this geometry to work reliably across the entire surface of the Earth at all times, the constellation must maintain a sufficient number of satellites distributed across well-defined orbital planes. Each individual spacecraft therefore plays a role not just as a standalone asset but as a component in a carefully coordinated global network.

GPS BIIF-6 belongs to the Block IIF generation of GPS satellites, which represented a significant modernization step in the evolution of the constellation. Block IIF satellites introduced a third civilian signal, known as L5, in addition to the legacy L1 and L2 signals that earlier generations transmitted. The L5 signal operates at a different frequency and is designed to support safety-of-life applications, particularly in aviation, where highly reliable and interference-resistant navigation signals are essential. Block IIF satellites also transmitted an improved version of the military M-code signal, enhancing performance for defense applications. Together, these enhancements made the Block IIF series meaningfully more capable than the Block IIA and Block IIR satellites they supplemented in the constellation.

The specific mission parameters for GPS BIIF-6 beyond its role as a standard GPS constellation member are not publicly detailed in available catalog records, and its current operational status is not confirmed in open sources. However, given its design and the nature of the program, it was built to contribute the same fundamental navigation and timing functions as its Block IIF siblings.

Orbit and Tracking

GPS BIIF-6 occupies a medium Earth orbit, the standard regime for GPS satellites and one carefully chosen to balance signal coverage geometry, signal travel time, and the engineering constraints of operating a large constellation. According to current tracking data, the satellite has an apogee of approximately 20,291 km and a perigee of approximately 20,088 km, making its orbit very nearly circular. The difference between those two figures — just over 200 km — is modest relative to the orbital altitude itself, meaning the spacecraft maintains a relatively consistent distance from Earth's surface throughout each revolution. Its orbital inclination is 55.6 degrees relative to the equatorial plane, which allows the satellite's ground track to sweep across both mid-latitude and high-latitude regions, ensuring that the constellation provides adequate coverage from the tropics to well into the polar regions.

The orbital period of GPS BIIF-6 is approximately 718.0 minutes, which works out to roughly eleven hours and fifty-eight minutes per revolution. This is not accidental. GPS satellites are designed to complete exactly two orbits for every one rotation of the Earth (accounting for the Earth's own motion around the Sun, this is measured relative to the sidereal day). This half-sidereal-day orbital resonance means that a given GPS satellite passes over the same ground locations at the same local time on successive days, which greatly simplifies the design of the constellation's coverage geometry and aids in predicting satellite availability for users at fixed locations.

The satellite is tracked under NORAD catalog number 39741 and can be followed using two-line element sets published by space surveillance networks. Because its orbit is well above low Earth orbit and it carries no exceptionally bright reflective surfaces, GPS BIIF-6 is not among the satellites most readily visible to casual observers with the naked eye, though it can in principle be detected with optical instruments under favorable conditions.

Design and Operator

GPS BIIF-6 was manufactured by Boeing, which was awarded the Block IIF production contract and delivered all twelve satellites in the series over a span of several years. Boeing's involvement in GPS production represented a continuation of the company's long history as a supplier to the United States military space program. The Block IIF satellites were larger and more capable than their predecessors, incorporating atomic clocks of improved stability — a critical element given that the entire GPS ranging system depends on extraordinarily precise timekeeping aboard each spacecraft. Rubidium and cesium atomic clocks were carried on each Block IIF satellite, and the upgraded clock performance translated directly into improved signal accuracy for end users.

The operator of the GPS constellation, including GPS BIIF-6, is the United States Air Force, specifically through the Space and Missile Systems Center (and, following organizational changes, the Space Force's Space Systems Command). Day-to-day management of the constellation, including uploading updated navigation messages to each satellite and monitoring spacecraft health, is conducted through the GPS Master Control Station located at Schriever Space Force Base in Colorado.

The mass of GPS BIIF-6 is not publicly confirmed in the available catalog data. Block IIF satellites as a class were substantially heavier at launch than earlier GPS generations, requiring larger launch vehicles, but the specific figure for this individual spacecraft is not recorded in open sources referenced here.

Launch and Deployment

GPS BIIF-6 lifted off on May 16, 2014, marking its entry into the operational constellation. The launch took place in the evening hours on the United States East Coast, at 20:00 Eastern Daylight Time. The satellite was assigned the international designator 2014-026A, indicating that it was the primary payload of the twenty-sixth launch event of 2014 as tracked by international convention. Following launch and on-orbit checkout — a process that typically involves verifying the health of all satellite systems, testing signal transmission, and confirming clock performance — Block IIF satellites were generally declared operational and integrated into the active constellation. The satellite has remained in orbit continuously since its launch and has not undergone any recorded decay or reentry.

Significance within the Block IIF Program

The Block IIF series as a whole occupied an important transitional position in the history of GPS. By the time GPS BIIF-6 launched in 2014, the program was simultaneously completing the IIF constellation and developing the next-generation Block III satellites. The twelve Block IIF satellites were deployed to replenish and modernize a constellation that had been sustaining operations with aging Block IIA satellites for many years, and their introduction of the L5 signal laid the groundwork for eventual multi-frequency civilian receivers capable of much higher accuracy than earlier single-frequency devices allowed. GPS BIIF-6, as the sixth satellite of twelve in the series, arrived at a point when the Block IIF deployment was well past its midpoint, helping to consolidate the improvements the series brought to the overall constellation.

Because GPS underpins an enormous range of modern infrastructure — from financial transaction timestamping and telecommunications network synchronization to precision agriculture, autonomous vehicle navigation, and emergency response — each satellite in the constellation carries systemic importance beyond its individual specifications. GPS BIIF-6 is one node in a network whose continuous availability is treated as critical infrastructure by the United States government and by the many nations and industries that depend on it.

The satellite's current operational or reserve status is not confirmed in publicly available catalog records. Block IIF satellites are designed with extended service lives, and it is common for GPS spacecraft to remain available in the constellation as active or reserve assets well beyond initial operational phases. Whether GPS BIIF-6 is currently transmitting navigation signals as an active constellation member, held in reserve, or in another operational state is not documented in the sources available to this record.

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