COSMOS 2251

Kosmos-2251 was a defunct Russian Strela-2M military communications satellite, inactive since the mid-1990s. On 10 February 2009 it collided with the active US Iridium 33 satellite at about 789 km over northern Siberia — the first accidental hypervelocity collision between two intact satellites. The Kosmos-2251 cloud is the larger of the two, with roughly 1,600 catalogued fragments.
About COSMOS 2251
Cosmos 2251 (also catalogued under the international designator 1993-036A and NORAD ID 22675) is a defunct Russian military communications satellite that has remained in low Earth orbit since its launch in June 1993. Once part of a Cold War–era network designed to relay military message traffic, the satellite outlasted its operational life by decades and became the subject of international attention following a catastrophic collision in 2009 that produced one of the largest debris fields in orbital history. Today the spacecraft itself remains aloft, a silent relic whose continued presence in a well-trafficked orbital band stands as a case study in the long-term consequences of leaving decommissioned satellites in place.
Mission and Purpose
Cosmos 2251 was a Strela-2M satellite, a class of Soviet-designed military communications spacecraft developed to serve the information relay needs of the Russian armed forces. The Strela ("Arrow") program traced its origins to the Soviet era, when the USSR pursued a variety of low Earth orbit satellite constellations to support secure military communications across its vast territory and fleet. The Strela-2M variant was a store-and-forward messaging system: rather than providing real-time relay links, satellites of this type would collect data uplinked from ground stations as they passed overhead, then retransmit it to another station later in their orbit. This approach was well suited to the era's constraints on onboard electronics and ground infrastructure, enabling the military to move message traffic without dependence on continuous line-of-sight links or geostationary relays.
The satellite was launched on June 16, 1993, carried atop a Kosmos-3M rocket from Launch Site 132/1 at the Plesetsk Cosmodrome, a high-latitude launch facility in northwestern Russia that has long served as the primary site for Russian military satellite launches. The Kosmos-3M was a reliable two-stage liquid-propellant rocket that served as the standard workhorse for lightweight Soviet and Russian military payloads throughout this period. Cosmos 2251's launch placed it under the operational authority of what is now the Russian Space Forces.
The expected service life for Strela-2M satellites was approximately five years, and by the Russian government's own account, Cosmos 2251 ceased functioning in 1995, roughly two years after launch. No mission-specific details about its operational record are publicly available in the satellite catalog, and the specifics of what communications it may have relayed during its brief active period remain undisclosed.
Orbit and Tracking
Cosmos 2251 operates in low Earth orbit at an inclination of 74.0 degrees, a high-inclination orbit well suited to providing coverage across the broad latitudes of Russian territory, including its Arctic regions. This orbital geometry allowed the satellite, during its active life, to pass over a wide swath of the globe in the course of each day. At an inclination significantly higher than the equatorial plane but short of a polar orbit, the satellite traces ground tracks reaching into sub-Arctic latitudes on every pass.
Current tracking data places the satellite at an apogee of approximately 803 kilometers and a perigee of approximately 768 kilometers, giving it a nearly circular orbit with relatively little eccentricity. The orbital period is 100.4 minutes, meaning the spacecraft completes roughly fourteen orbits of Earth each day. At these altitudes, atmospheric drag is low enough that orbital decay is a very slow process; the satellite has shown no sign of imminent reentry and remains catalogued as still in orbit.
The orbit it occupies is not an isolated one. The altitude band between roughly 700 and 900 kilometers is among the more congested regions of near-Earth space, hosting a large number of operational satellites, spent rocket stages, and debris objects. It was precisely this crowding that contributed to the circumstances of the 2009 collision. Tracking of Cosmos 2251 is maintained by United States Space Command, which publishes two-line element sets for the object under NORAD catalog ID 22675, allowing observers and conjunction analysts to monitor its position.
Design and Operator
Cosmos 2251 is classified as a payload object with a catalogued mass of approximately 900 kilograms. It belongs to the KAUR-1 spacecraft bus family, a Soviet-era satellite platform used across several low Earth orbit military satellite programs. One of the defining characteristics of the KAUR-1 bus that is directly relevant to Cosmos 2251's post-operational history is that satellites built on this platform were not equipped with any onboard propulsion system. Without thrusters, the satellite had no capability to raise or lower its orbit, execute collision-avoidance maneuvers, or perform a controlled deorbit at the end of its service life.
The manufacturer of Cosmos 2251 is not publicly recorded in the available catalog data. The satellite was operated by the Russian Space Forces, the branch of the Russian military responsible for the launch, operation, and tracking of military space assets. Russia has not released detailed technical specifications for the Strela-2M series beyond what has entered the public domain through general historical accounts of Soviet military space programs.
The absence of propulsion was not an unusual design choice for the era. Many Soviet military satellites of the 1970s, 1980s, and early 1990s were designed with defined operational lifespans and were not intended to be maneuvered after their missions concluded. The expectation was that atmospheric drag would eventually bring such satellites down naturally, though at altitudes above 700 kilometers this process unfolds over timescales measured in decades or longer rather than years.
Significance and Legacy
Cosmos 2251 became globally significant on February 10, 2009, when it collided with Iridium 33, an active commercial communications satellite operated by Iridium Communications. The collision occurred at high relative velocity at an altitude of approximately 789 kilometers — well within the orbital band where Cosmos 2251 was circling — and the impact destroyed both satellites entirely. The event generated an enormous cloud of debris fragments, numbering in the thousands of trackable pieces and far more untrackable smaller particles, distributed across a range of orbital altitudes. It was the first accidental hypervelocity collision between two intact satellites ever recorded, and it significantly worsened the debris environment in low Earth orbit for years afterward.
The incident drew renewed scrutiny to the practice of leaving defunct satellites in operational orbits. The Space Review, among other outlets and analysts, criticized Russia for not having deorbited Cosmos 2251 after it stopped functioning in 1995, arguing that leaving a large, inert mass in a crowded orbital region for over a decade created unnecessary collision risk. Russia responded that no binding obligation under international space law required it to remove the satellite, a position that was technically accurate under the frameworks then in place. The episode accelerated discussions within the international spacefaring community about the need for stronger debris mitigation guidelines and, eventually, active debris removal capabilities.
The collision also reinforced a broader lesson that has shaped modern satellite design and operations: passive disposal — waiting for atmospheric drag to eventually bring a spacecraft down — is inadequate in high-altitude low Earth orbit on any practical timescale. Many regulatory bodies and standards organizations have since refined guidelines recommending that satellites in low Earth orbit be deorbited within 25 years of end of mission, though implementation and enforcement remain inconsistent across operators and jurisdictions.
For tracking purposes, Cosmos 2251 itself remains in orbit under its original catalog identifier, distinct from the extensive debris catalog entries created by the collision. Its continued orbital presence, more than thirty years after launch, is a concrete illustration of just how long objects can persist at these altitudes without any active intervention. The original spacecraft, now a lifeless hulk of approximately 900 kilograms, continues to circle Earth roughly once every hour and forty minutes, invisible to the naked eye in most circumstances and posing an ongoing if statistically small collision risk to other objects sharing its orbital neighborhood.
How to Spot It
Cosmos 2251 is not generally considered a bright naked-eye target, and it does not appear on standard lists of easily observable satellites. At roughly 800 kilometers altitude in a 74-degree-inclination orbit, it is geometrically accessible to observers across a very wide range of latitudes — essentially anywhere between about 74 degrees north and 74 degrees south can see it pass overhead given the right timing. However, with no large reflective surfaces such as solar array panels or antennas of the kind that make some satellites conspicuous, the object tends to be faint.
Observers equipped with binoculars and using up-to-date tracking predictions based on the current NORAD two-line element set for catalog ID 22675 may be able to identify it as a slowly moving point of light during twilight passes, when the satellite is illuminated by sunlight while the observer is in darkness. Dedicated satellite-spotting tools that accept catalog IDs can generate precise pass predictions for any observing location. Given its status as a debris-generating historical object, it holds particular interest for observers who follow the history of space situational awareness and orbital safety.
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