Swift boost mission
On-orbit satellite servicing mission
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The Swift boost mission is a robotic on-orbit satellite servicing mission to boost the orbit and extend the lifetime of the Neil Gehrels Swift Observatory, which is otherwise anticipated to undergo uncontrolled reentry by the end of 2026. The LINK servicing spacecraft, built and operated by Katalyst Space Technologies, was launched on July 3, 2026. As of July 28[update], LINK is undergoing an attempted recovery from an attitude control and propulsion malfunction during commissioning that may jeopardize its mission.[7]
- LINK: Katalyst Space Technologies[1]
- Swift: NASA/Pennsylvania State University[2]
LINK being prepared for thermal vacuum testing | |
| Mission type | On-orbit satellite servicing |
|---|---|
| Operator |
|
| COSPAR ID | 2026-152A |
| SATCAT no. | 69792 |
| Website | science |
| Mission duration | 42 days, 13 hours, 42 minutes (elapsed) |
| Spacecraft properties | |
| Spacecraft | LINK |
| Manufacturer | Katalyst Space Technologies |
| Launch mass | 425 kg (937 lb)[3] |
| Dry mass | 365 kg (805 lb)[3] |
| Dimensions | Height: 1.5 m (4.9 ft) Deployed width: 6 m (20 ft)[4] |
| Power | 40 kW[4]: 11:00 |
| Start of mission | |
| Launch date | July 3, 2026, 08:36 UTC[5] |
| Rocket | Pegasus XL |
| Launch site | Kwajalein Atoll |
| Contractor | Northrop Grumman |
| Orbital parameters | |
| Reference system | Geocentric orbit |
| Regime | Low Earth orbit |
| Perigee altitude | 362 km (225 mi) (initial)[6] |
| Apogee altitude | 392 km (244 mi) (initial) |
| Inclination | 20.6° |
| Capture of Neil Gehrels Swift Observatory | |
| RMS capture | TBD |
| RMS release | TBD |
| Time captured | TBD |
Katalyst mission patch, with Latin motto "Audentes fortuna iuvat" ("Fortune favors the bold") | |
If successful, LINK will be the first commercial spacecraft to dock with a government-owned spacecraft that was not designed for docking or on-orbit servicing.[8][9]
Swift
Swift is a three-instrument gamma-ray observatory launched in 2004.[10] It monitors gamma-ray bursts (GRBs), detecting about one hundred per year[1] and providing data to other observatories.[8] Swift has cost $500 million to build, launch, and operate as of 2026[update].[11] It has a unique ability to quickly turn to observe GRBs before they fade,[11] and with no planned replacement, its loss would significantly impede time-domain astrophysics.[9][1]

Swift occupies a low Earth orbit with an original altitude of approximately 600 kilometers (370 mi), which has decayed since launch to approximately 400 kilometers (250 mi) due to atmospheric drag.[10] Increased solar activity around the 2024 solar maximum expanded the Earth's atmosphere and accelerated the decay,[11] with uncontrolled reentry anticipated by the end of 2026.[8][9] Swift does not have a propulsion system of its own.[10]
Contract award
In August 2025, NASA awarded two companies, Cambrian Works and Katalyst Space Technologies, $150,000 each under Phase III SBIR contracts for concept design studies for a Swift orbit boost mission.[12] In September, NASA awarded Katalyst with a $30 million SBIR Phase III contract to develop and launch a spacecraft to dock with Swift and boost its orbit.[8] Katalyst beat out proposals from Starfish Space and a joint venture of Cambrian Works and Astroscale. In the award announcement, NASA official Shawn Domagal-Goldman said "Given how quickly Swift's orbit is decaying, we are in a race against the clock" to save it.[8]
The $30 million contract is a very modest sum for the development and launching of a spacecraft;[13][14][15] by comparison, Swift cost $250 million to build and launch in 2004.[15] A Northrop Grumman Pegasus launch cost $28 million in 2021,[11] though Katalyst reportedly obtained launch services from Northrop at a discount; the Pegasus used to launch LINK was originally built for another customer.[16]
Katalyst, founded in 2020 and based in Flagstaff, Arizona was already planning a mission in 2026 to demonstrate its on-orbit servicing capability.[11] The company has not previously flown a spacecraft, but Atomos Space, which Katalyst acquired in April 2025, has.[17] The company will use the Swift rescue mission to reduce the technical risk of its planned geostationary multi-mission servicing spacecraft, NEXUS, planned for 2027.[9][18]
The selection of a private enterprise for the Swift rescue mission represents a policy shift for NASA with respect to servicing in low Earth orbit, following the 2024 cancellation of the in-house OSAM-1 (formerly Restore-L) mission due to cost overruns.[1][19]
Drag minimization
Since February 11, 2026, most of Swift's science operations have been suspended in favor of pointing the spacecraft and its solar arrays to minimize drag and extend the orbit lifetime.[20] By disabling instruments and relaxing a requirement to have its solar arrays pointing within ten degrees of the Sun, Swift's operators have been able to reduce its average cross-sectional area in the direction of flight by approximately thirty percent while remaining power positive.[21] If Swift slips below approximately 300 km (190 mi), drag forces may make it impossible for the servicing spacecraft to dock and maintain control.[11] As of mid-June[update], modeling predicted Swift will remain above this critical altitude into at least October, three to four months beyond what was predicted prior to drag minimization efforts, leaving sufficient time for LINK to rendezvous and dock.[4]: 23:00
LINK development
Development of Katalyst's LINK spacecraft occurred under a greatly accelerated timeline,[8][18] with environmental testing at Goddard completed on May 4, 2026, just eight months after contract award,[10][8] and launch occurring two months later; a comparable mission would typically have a development time of twenty-four months from award to launch.[18] Following environmental testing, the spacecraft returned to Katalyst's Broomfield, Colorado facility for additional testing.[10] The Pegasus air-launch system was selected partly for its ability to launch into Swift's low, 20.6 degree inclination.[22]
LINK launch and commissioning

On June 5, the spacecraft arrived at Wallops Flight Facility in Virginia to be mated to the Pegasus XL rocket. Integration of the spacecraft and rocket was completed on June 9,[23] mating of the rocket to the Stargazer aircraft was completed on June 12,[24] and Stargazer departed Wallops on June 18 for the launch site at Kwajalein Atoll in the Marshall Islands,[25] arriving June 25.[26] Following launch scrubs for weather on June 30[27] and July 1,[28] and a scrub for a technical issue with the launch vehicle on July 2,[29] the spacecraft was successfully launched on July 3, 2026, at 08:36 UTC.[5] This was the last planned launch of a Pegasus rocket.[5][30] Katalyst confirmed the day after launch that the spacecraft deployed successfully, and checkouts and commissioning had begun.[31]
On July 15, twelve days after launch, NASA reported that spacecraft commissioning was about half complete, with power systems and avionics commissioned, and propulsion system checkouts performed. Early issues with communications and attitude control were addressed with patches to flight software and updates to operating procedures.[32]
Attitude control failure and recovery
On July 25, LINK lost attitude control and began to tumble, causing communications failures and a bus reset. Once communication was restored, analysis determined that two of the vehicle's three reaction wheels were not operable, and its cold gas thruster system was also degraded. The spacecraft remained able to generate sufficient power, and its operations team began working to stop the spin using one of the vehicle's two-axis gimballed electric thrusters.[33][34]
LINK's spin was incrementally slowed from an initial nine degrees per second to 1.47 degrees per second as of August 5, where it remained while preparations continued for the next phase of the mission.[34] Less than 100 grams (3.5 oz) of propellant were consumed to control the spin, out of the 60 kilograms (130 lb) LINK launched with.[34][3] Katalyst also began working with NASA to develop a new attitude controller to adjust for the degraded state of the vehicle.[34] This new controller was uplinked on August 11, allowing Katalyst to begin a series of maneuvers to align LINK's orbit with Swift's.[34]
The reaction wheel failures were reportedly caused by a temperature spike in their control electronics, resulting from the hard bus reset that occurred automatically after twenty-four hours without contact. The cause of the original spin had not been determined as of August 1[update]. Katalyst expected to be able to downlink additional data on its condition, including photographs to determine whether the vehicle was struck by space debris.[35] As of August 11[update], no root cause has been announced.[36]
Katalyst CEO Ghonhee Lee said on August 1: "As it stands right now, we have not made a formal assessment, but we believe that a capture of Swift, an attempted capture of Swift, is very much in the cards."[35] Katalyst and NASA will jointly assess the safety of the new approach and capture plan.[37] Recovery efforts will delay any rendezvous until late August at the earliest.[34]
Rendezvous, capture, and boost

Katalyst originally anticipated post-launch vehicle checkouts to take two weeks, followed by two to three weeks for rendezvous and inspection of Swift, and one to two weeks for close approach and capture.[38] A malfunction of LINK's attitude control system, and subsequent recovery efforts, have delayed this timeline, with rendezvous now anticipated in late August, around eight weeks after launch.[34]
LINK is equipped with three parallel manipulator robotic arms, described as a "split Stewart platform",[4] each equipped with lidar sensors and three-degree-of-freedom grippers.[39][22] The boost can be performed with capture by one arm, but three offer better control.[4]: 40:00
Swift was not designed for on-orbit servicing, and does not have a docking port or grappling fixtures. Instead, LINK will attempt to attach to ground-handling flanges on the bus.[1][39] Upon approaching within tens of meters, the two spacecraft will perform tandem operations to allow for visual inspection of the intended and backup gripping points, to ensure they are unobstructed (such as by torn multi-layer insulation) before attempting to dock.[22][4]: 38:00 No close-out photographs of Swift's base are available,[22] and prior experience with servicing missions to Hubble revealed that multi-layer insulation may become embrittled in the space environment, leading it to shatter on contact, which would risk damaging Swift.[4]: 41:00
The docking procedure was validated in a robotic testbed on an air bearing table, with a full-scale model of Swift's base.[4]: 46:00 Swift is described as "unprepared but cooperative" in that it is capable of coordinated attitude control to assist with inspection and docking.[4]: 43:00 The docking procedure includes several go/no-go decision points requiring approval of both vehicles' operations teams, with the ability to abort and retry if necessary.[4]: 47:00
Once docked, LINK will raise Swift's orbit over a period of about three months,[38] using three Hall-effect thrusters with xenon propellant, gimballed to align with the center of mass of the stacked vehicles,[22][40][41] as well as sixteen reaction control system thrusters.[4]: 11:00 LINK will perform attitude control for the stack,[42] despite being significantly less massive, at 425 kg (937 lb), than Swift, at 1,470 kg (3,240 lb).
Following the boost, LINK will undock and distance itself from Swift, which will require about a month for recommissioning before returning to science operations.[38] LINK will potentially pursue additional test objectives. Before passivation, LINK will use its remaining fuel to decrease its altitude in order to accelerate its reentry.[4]
Swift mission director John Van Eepoel has said "The Swift boost attempt is a fast, high-risk, high-reward mission".[10] If successful, Swift's operational life is expected to be extended by at least ten years.[22]
See also
- 2026 in spaceflight
- Mission Extension Vehicle, a more complex vehicle intended to service spacecraft in geosynchronous orbit
- Robotic Servicing of Geosynchronous Satellites program