AEHF-4 (USA 288)

NORAD 43651· COSPAR 2018-079A· Active satellite· Communications· GEO
Launch
Launched on Oct 17, 2018 from Space Launch Complex 41, United States of America aboard a Atlas V 551.
Atlas V 551 | AEHF-4 (USA 288)
AEHF-4 (USA 288)
USAF (Los Angeles AFB) · Public domain · via Wikimedia Commons
Live · TLE epoch 2026-07-13 13:08 UTC
Orbit class
GEO — Geostationary (~35,786 km, equatorial)
Operator
United States Space Force
Country
United States
Manufacturer
Lockheed Martin Space
Launched
Oct 17, 2018
Mass
6,168 kg
Apogee
36,040 km
Perigee
35,546 km
Inclination
1.44°
Period
23.93 h

About AEHF-4 (USA 288)

AEHF-4, catalogued by NORAD as object 43651 and internationally designated 2018-079A, is a military communications satellite launched on October 16, 2018. Also referred to by its cover designation USA-288, it represents the fourth spacecraft to reach orbit as part of the United States military's Advanced Extremely High Frequency (AEHF) program. Built by Lockheed Martin Space and now operated by the United States Space Force, the satellite occupies a near-geostationary orbit and forms a key node in a constellation designed to provide survivable, protected communications for the nation's highest-priority military users.

Mission and Purpose

The AEHF program exists to provide strategic and tactical communications that remain functional even in severely contested electromagnetic environments — including scenarios involving nuclear detonations, deliberate jamming, and other forms of electronic warfare. It was developed as the successor to the Milstar satellite system, inheriting Milstar's core mission of hardened, low-probability-of-intercept communications while offering substantially greater throughput and flexibility.

AEHF satellites serve the command-and-control needs of national leadership and senior military commanders, carrying voice, data, and video traffic for users across the United States and its allies. The system is designed to interoperate with allied terminals, extending protected communications to partner nations who have invested in compatible ground infrastructure. The satellites operate across Extremely High Frequency (EHF) bands, which offer natural resistance to jamming and a reduced electromagnetic footprint compared to lower-frequency systems, making transmissions considerably harder for adversaries to detect or disrupt.

The specific mission parameters of AEHF-4 are not publicly disclosed in the satellite catalog, and its precise orbital slot and payload configuration remain classified. What is known is that it follows the same general design philosophy and mission framework as the first three satellites in the constellation, filling in coverage gaps and adding redundancy to the network. Together, the constellation of AEHF satellites was intended to replace Milstar on a one-for-one basis and then expand the architecture's capability further with additional vehicles.

Orbit and Tracking

AEHF-4 operates in a geostationary — or very nearly geostationary — orbit, a band of space roughly 35,000 kilometers above Earth's equator where a satellite's orbital period matches the planet's rotation rate. At that altitude, a spacecraft appears essentially stationary relative to ground-based observers and antennas, making it ideal for continuous communications coverage over a fixed region of the globe.

The tracked orbital elements for AEHF-4 place its apogee at 36,049 km and its perigee at 35,539 km, giving an orbit that is very nearly circular but with a small amount of residual eccentricity. Its inclination is measured at 1.4°, a slight departure from the ideal 0° of a perfectly geostationary orbit, which means the satellite traces a small figure-eight pattern — known as an analemma — when its apparent position is plotted over time from a fixed Earth location. This minor inclination is characteristic of operational geosynchronous spacecraft that have used some but not all of their stationkeeping propellant, or that are being managed in a slightly inclined orbit for operational reasons. The orbital period of 1,436.1 minutes is extremely close to one sidereal day, confirming its placement in the geostationary belt.

AEHF-4 carries the NORAD catalog identifier 43651. It is tracked routinely by the United States Space Surveillance Network and appears in public orbital element catalogs, though the satellite itself — as with most military payloads — is not explicitly labeled with its operational function in those records. The object was launched into its current orbital class and has remained in orbit without any recorded reentry or decay event.

Design and Operator

AEHF-4 was manufactured by Lockheed Martin Space, a division of the Lockheed Martin Corporation that has long been one of the primary contractors for high-value national security space systems. The AEHF satellites are based on Lockheed Martin's A2100 satellite bus, a large, three-axis-stabilized platform designed for long-duration geosynchronous missions. The A2100 bus has an established heritage in both commercial and government applications, prized for its modular design and capacity to accommodate substantial payloads.

The satellite has a launch mass of 6,168 kg, placing it firmly in the category of large geosynchronous payloads. Satellites of this mass class typically require powerful launch vehicles to place them in or near geostationary transfer orbit, and they generally carry considerable onboard propellant to complete the final orbit-raising maneuvers after separation from the rocket. AEHF satellites are known for their extended operational design lives, consistent with the investment required for protected military communications infrastructure.

Operational control of AEHF-4 rests with the United States Space Force, the branch of the U.S. armed forces established in December 2019 to manage military space operations. At the time of its launch, the program was administered under the United States Air Force — the Space Force's parent institution — but jurisdiction transferred when the new service branch was created. Day-to-day satellite operations are conducted through Space Force units specializing in protected satellite communications, with the broader program managed in coordination with the Space and Missile Systems Center and related acquisition authorities.

The AEHF program was developed as a joint effort, with funding and participation from allied nations. Canada, the Netherlands, and the United Kingdom have all been partners in the program, contributing resources in exchange for access to the communications capacity the constellation provides. This multinational character distinguishes AEHF from some purely national satellite programs and reflects the broader interoperability goals of Western military communications architectures.

Program Context and Significance

AEHF-4 is the fourth of six satellites planned for the AEHF constellation. The first satellite was launched in 2010, followed by subsequent vehicles that gradually built out the constellation's global coverage. The addition of AEHF-4 in 2018 contributed meaningfully to the redundancy and capacity of the network, ensuring that the loss or degradation of a single satellite would not create a critical gap in coverage.

The transition from Milstar to AEHF represented a significant leap in military communications capability. Milstar, while groundbreaking at the time of its development, was limited in data throughput by the standards of later communications requirements. The AEHF system was designed to deliver dramatically higher data rates while preserving and extending the survivability characteristics that made Milstar valuable — particularly the ability to maintain connectivity in a nuclear or high-interference environment.

The broader geopolitical context for systems like AEHF has grown more pressing over time. Adversarial development of anti-satellite weapons, directed energy systems, and sophisticated jamming capabilities has placed increased emphasis on the "protected" nature of communications satellites. AEHF's design philosophy, emphasizing resistance to nuclear effects, jamming, and interception, reflects the enduring military judgment that some communications links must function regardless of what an adversary does to the electromagnetic environment or the space domain.

AEHF-4's launch in 2018 came at a period of renewed strategic attention to space as a contested domain. The year prior, the U.S. Department of Defense had begun articulating more explicitly that space was no longer a sanctuary, and the importance of resilient, survivable architectures like AEHF was being underscored in public strategy documents. The satellite thus arrived in orbit at a moment when the mission it embodies was receiving heightened institutional and budgetary attention.

Current Status

AEHF-4 remains in orbit as of the time of this entry, with no decay or reentry recorded in the catalog. Its operational status is not publicly disclosed, as is standard for classified military communications payloads. Based on the orbital parameters on record, the satellite continues to occupy a near-geostationary position consistent with active service in the AEHF constellation.

The United States Space Force, as the current operator, does not release status reports or operational updates for individual AEHF satellites through public channels. Whether the satellite is in active operational service, held in reserve, or undergoing any particular phase of its mission life is not verifiable from publicly available sources. Its continued presence in the geostationary belt, however, is confirmed by ongoing tracking data.

As the AEHF constellation matures and successor programs such as the Protected Tactical Satcom (PTS) and the next-generation protected communications architecture move through development, satellites like AEHF-4 are expected to continue serving as the backbone of U.S. and allied protected military communications for the foreseeable future. The program's satellites are designed for long operational lives, and AEHF-4, launched in 2018, should have considerable service life remaining by most reasonable assessments of its design parameters.

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