FLYING LAPTOP

NORAD 42831· COSPAR 2017-042G· ISS / Science· SSO
Launch
Launched on Jul 14, 2017 from 31/6, Kazakhstan aboard a Soyuz 2.1a Fregat-M.
Soyuz-2.1a/Fregat | Kanopus-V-IK
Live · TLE epoch 2026-07-13 13:55 UTC
Orbit class
SSO — Sun-Synchronous (LEO at 96–102° inclination)
Operator
DLR
Country
Germany
Manufacturer
Launched
Jul 14, 2017
Mass
120 kg
Apogee
581 km
Perigee
553 km
Inclination
97.48°
Period
1.60 h

About FLYING LAPTOP

Flying Laptop (NORAD 42831, COSPAR 2017-042G) is a German small satellite developed under the auspices of DLR, the German Aerospace Center, and launched into a Sun-synchronous orbit in July 2017. Weighing approximately 120 kilograms, it represents a class of compact yet scientifically ambitious spacecraft that emerged from the growing small-satellite movement of the 2010s, when advances in miniaturized electronics and modular design allowed universities and national space agencies alike to pursue meaningful orbital research at a fraction of the cost of traditional missions. The satellite carries a laser communications payload that places it at the intersection of cutting-edge optical communications research and the broader ambition to modernize how spacecraft exchange data with the ground.

Mission and Purpose

Flying Laptop's most notable feature is that it hosts the OSIRISv1 laser communications experiment, an optical inter-satellite and satellite-to-ground communications demonstrator. Traditional satellite communications rely on radio frequency links, which face growing pressure from spectrum congestion as the number of orbiting platforms increases. Optical, or laser-based, communication systems offer a compelling alternative: they can carry substantially more data per unit of bandwidth, are inherently more difficult to intercept, and do not require internationally coordinated radio frequency licenses. OSIRISv1 was designed to test and validate this technology in a real orbital environment, collecting performance data that could inform future operational systems.

Laser communication from low Earth orbit presents considerable engineering challenges. The satellite and any ground station are in relative motion at several kilometers per second, so the laser beam — which is extraordinarily narrow compared with a radio beam — must be precisely pointed and tracked in real time. Atmospheric turbulence, cloud cover, and pointing jitter all degrade link performance in ways that are difficult to fully replicate in ground-based laboratories. Flying Laptop's mission thus served a dual purpose: it generated scientifically useful measurements about optical propagation through the atmosphere, and it stress-tested the hardware and software algorithms that would need to be refined before laser communications could be deployed on operational satellites.

Beyond the laser communications experiment, the spacecraft was intended to provide operational experience in managing a small satellite platform through a realistic mission lifecycle — from commissioning through regular operations. The specific details of any secondary payloads or instruments are not publicly recorded in the satellite catalog, so only the laser communications role can be confirmed from available data.

Orbit and Tracking

Flying Laptop occupies a Sun-synchronous orbit (SSO), a class of near-polar orbit in which the satellite's orbital plane precesses at the same rate that Earth moves around the Sun — approximately one degree per day. The practical consequence is that the spacecraft passes over any given latitude at the same local solar time on each successive orbit, ensuring consistent illumination conditions for sensors and predictable thermal cycling for the platform. Sun-synchronous orbits are a standard choice for Earth observation and technology demonstration missions because they simplify mission planning and ground operations.

According to current tracking data, Flying Laptop has an apogee of 581 km and a perigee of 554 km, placing it in a slightly elliptical low Earth orbit with a mean altitude broadly consistent with the low-600-kilometer range typical of SSO platforms. Its inclination is 97.5°, which is the retrograde tilt that produces the Sun-synchronous precession. The orbital period is approximately 95.9 minutes, meaning the satellite completes roughly fifteen orbits of Earth each day.

The satellite was launched on 13 July 2017 (UTC offset depending on time zone; the launch occurred on 14 July 2017 local time at the launch site) aboard a Soyuz-2.1a rocket from the Baikonur Cosmodrome in Kazakhstan. Baikonur, one of the world's oldest and most active launch facilities, has supported a wide variety of international payloads, and the Soyuz-2.1a vehicle is a workhorse of medium-lift launches with an extensive heritage of successful missions. Flying Laptop was one of several payloads sharing the launch, as is common for SSO rideshare missions.

As of the most recent catalog update, Flying Laptop remains in orbit and has not experienced decay or reentry. At its current altitude band, atmospheric drag is present but modest, and a spacecraft of this type can remain in orbit for a substantial number of years before natural deorbit. Continuous tracking by ground-based radar networks maintains its catalog entry, and its two-line element sets are regularly updated to reflect the slow evolution of its orbital parameters.

Design and Operator

Flying Laptop has a mass of 120 kg, placing it firmly in the category of small satellites — large enough to accommodate meaningful payloads and power systems, but small enough to fly as a secondary payload on a commercial rideshare. The satellite was developed under DLR, Germany's national space agency and aeronautics research center. DLR operates a broad portfolio spanning aviation, space transportation, energy, and security research, and it has a long record of developing and operating scientific satellites as well as supporting German contributions to European Space Agency programs.

The manufacturer of Flying Laptop is not listed in the publicly available satellite catalog, so this detail cannot be confirmed here. DLR satellites in this class have historically involved collaborations with universities and industrial partners, reflecting the agency's commitment to training the next generation of space engineers while advancing applied research. The Flying Laptop project in particular has been associated with the University of Stuttgart's Institute of Space Systems, a connection that fits the broader pattern of DLR-affiliated academic institutions developing hands-on spacecraft as a training and research vehicle — hence the informal but evocative name "Flying Laptop," suggesting a capable, programmable platform compact enough to be treated with the informality of a personal computer.

The satellite's country of ownership is Germany, and it operates under German jurisdiction in accordance with international space law, including registration obligations under the UN Registration Convention.

Significance and Current Status

Flying Laptop represents a meaningful contribution to the development of optical communications technology for space applications. The OSIRISv1 experiment placed an operational laser link terminal in orbit at a time when most laser communication demonstrations were either ground-based, on large government platforms, or in experimental configurations not designed for sustained operations. Demonstrating the technology on a small, relatively low-cost satellite helped establish that optical communications was not confined to large flagship missions, and that the engineering challenges — pointing, acquisition, atmospheric compensation — could be managed within the constraints of a compact platform.

More broadly, Flying Laptop is part of a generation of small satellites that reshaped expectations about what a modestly resourced program could accomplish. Through the 2010s, the success of small satellite missions in conducting genuine science and technology demonstration — rather than simply proving that a small satellite could survive in orbit — encouraged further investment in the sector and contributed to the proliferation of small satellite constellations that have come to define commercial space in the early 2020s.

The satellite's current operational status is not definitively recorded in the public catalog, and no specific mission conclusion date is available. It remains in orbit with a well-characterized set of orbital elements, and ground stations equipped for optical communications experiments may still be able to interact with it. Whether the spacecraft continues active operations or has transitioned to a passive state is not confirmed in available data.

The mission demonstrates the value of national space agency investment in small satellite platforms not only for their direct scientific return but also for the institutional knowledge and workforce development they generate. Engineers who work through the full lifecycle of a small satellite — from design and testing through launch, commissioning, and operations — develop skills that are directly transferable to larger and more complex programs.

How to Spot It

Flying Laptop is a 120-kilogram small satellite orbiting at altitudes between 554 and 581 km, and like most small satellites in this size class it is not among the brightest objects visible to the naked eye under typical conditions. However, it is not invisible: at favorable geometry — passes that occur during twilight, when the observer is in Earth's shadow but the satellite is still illuminated by sunlight — it may be detectable with modest optical aid such as binoculars or a small telescope. Its orbital period of 95.9 minutes and inclination of 97.5° mean it passes over a wide range of latitudes on each orbit, and observers at mid-latitudes in Germany and across Europe, as well as in many other regions, will see regular passes.

The most reliable way to identify and time passes is to use the current two-line element data available on this site, which reflects the most up-to-date tracking information from the global radar network. Prediction tools will calculate rise time, maximum elevation, and azimuth for any observer location, allowing you to plan an observation with accuracy of seconds. As with any satellite observation, the period roughly one hour after sunset or one hour before sunrise offers the best contrast between a sunlit satellite and a darkened sky.

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