Orbital debris
node
The population of non-functional objects in Earth orbit: spent upper stages, dead satellites, deliberately destroyed spacecraft, released hardware, and fragments from collisions, explosions and surface degradation. Space surveillance networks catalogue tens of thousands of objects large enough to track — broadly, above about ten centimetres in low Earth orbit — while statistical models put the number above one centimetre in the high hundreds of thousands to over a million, and the number above one millimetre in the hundreds of millions. The size distribution is what makes it dangerous: at closing speeds around ten kilometres per second an untrackable centimetre-scale fragment carries the kinetic energy of a small car at motorway speed, so the objects most likely to destroy a satellite are precisely the ones that cannot be avoided because they cannot be seen. Two deliberate anti-satellite tests and one accidental collision account for a large share of the catalogued fragments in low Earth orbit. The economic character of the problem is that it is a classic externality: the cost of a fragment falls on every future operator of that altitude band, not on whoever created it. Not a terrestrial place.
A node is not a place. Drawing it on a map would assert something about the world that no stored fact supports.
Read in · 1
Evidence · 3
Timeline
No dated observations are stored for this object. Atlas shows what was observed and when — it does not infer a history.
Connections · 1
Assembled narrative · 1
Assembled from 34 blocks · 3 evidence · 30 related
- Story
- The population of non-functional objects in Earth orbit: spent upper stages, dead satellites, deliberately destroyed spacecraft, released hardware, and fragments from collisions, explosions and surface degradation. Space surveillance networks catalogue tens of thousands of objects large enough to track — broadly, above about ten centimetres in low Earth orbit — while statistical models put the number above one centimetre in the high hundreds of thousands to over a million, and the number above one millimetre in the hundreds of millions. The size distribution is what makes it dangerous: at closing speeds around ten kilometres per second an untrackable centimetre-scale fragment carries the kinetic energy of a small car at motorway speed, so the objects most likely to destroy a satellite are precisely the ones that cannot be avoided because they cannot be seen. Two deliberate anti-satellite tests and one accidental collision account for a large share of the catalogued fragments in low Earth orbit. The economic character of the problem is that it is a classic externality: the cost of a fragment falls on every future operator of that altitude band, not on whoever created it. Not a terrestrial place.
- Knowledge
- Low Earth orbit broadband constellations
- Orbital debris
- Connections
- Low Earth orbit broadband constellations
- Low Earth orbit broadband constellations
- The Kessler collision cascade
- The FCC five-year post-mission disposal rule
- Kessler and Cour-Palais publish the collision cascade argument
- A Chinese anti-satellite test destroys the Fengyun-1C weather satellite
- The UN adopts voluntary space debris mitigation guidelines
- Iridium 33 and Cosmos 2251 collide
- The first sixty Starlink satellites are deployed
- A Russian anti-satellite test destroys Cosmos 1408
- The FCC adopts a five-year post-mission disposal rule
- Orbital debris
- ITU spectrum and orbital-slot regulation
- Orbital shells as distinct economic regimes
- Reusable orbital launch
- Satellite communications
- Orbital debris
- The FCC five-year post-mission disposal rule
- The first sixty Starlink satellites are deployed
- OneWeb files for bankruptcy protection
- The FCC adopts a five-year post-mission disposal rule
- OneWeb completes its first-generation constellation
- Amazon begins deploying production broadband satellites
- A constellation deployment milestone falls due
- Evidence
- Supports the catalogued and modelled debris population magnitudes, the altitude dependence of orbital decay, and the fragment contributions of the 2007 Fengyun-1C test, the 2009 Iridium–Cosmos collision and the 2021 Cosmos 1408 test. V55 verification basis: esa.int was refused by the network egress proxy in this session and no search was available, so counts are given as ranges and no edition-specific number is quoted.
- Sets out the collision-cascade mechanism by which a debris population becomes self-sustaining above a threshold density. V55 verification basis: the paper was not retrieved in this session; the issue and page range are deliberately omitted rather than stated from memory, and only the volume and year are given.
- Establishes voluntary, non-binding debris mitigation expectations including removal of low-Earth-orbit spacecraft within twenty-five years of mission end. V55 verification basis: the guidelines were not retrieved in this session; the adoption year and the twenty-five-year expectation are stated from author knowledge.
Observed changes · 0
No public Signals are attached to this object. Signals show what changed and when it was observed — never a direction or a rank.
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