Orbits

Every fragment comes back through the same point

When a satellite breaks up, its pieces fly off in every direction and every one of them returns, an orbit later, to the place where it broke. The cloud pinches there once a period, stretches along the orbit at a rate set by one component of each kick, and becomes a ring in hours.

Assumes Vis-viva and Orbital elements.

The vis-viva equation gives the speed of an orbiting body anywhere on its orbit, v2=μ(2/r−1/a)v^2 = \mu(2/r - 1/a), and the eccentricity is not in it. Read the other way, it says something just as striking: the semi-major axis of an orbit — and with it the orbit’s energy and period — is fixed by the speed at one point and the distance from the centre, and not by the direction the body is moving in. Two bodies at the same place with the same speed have the same period, whether one is moving along the old orbit and the other straight up.

That fact organises one of the most consequential events in orbit: a break-up. When a satellite explodes, or two satellites collide, or a missile destroys one, the fragments leave the break-up point in every direction with a spread of speeds, and each follows its own Kepler ellipse from then on. Vis-viva decides what the cloud does next, and the answer has three parts that are not obvious from the picture of a spray of debris: the cloud re-forms at the break-up point once a period, it stretches along the orbit at a rate set by one component of each kick, and it closes into a ring round the Earth in a time that can be computed on the back of an envelope.

A cloud of fragments that pinches where it was born. 240 fragments thrown from a satellite on a circular orbit 800 kilometres up, with kicks of about 100 metres a second in random directions in the orbital plane, each then following its own Kepler ellipse, drawn at 0.5, 1, 4.5, 20 orbital periods of the parent, with the Earth's centre marked and the break-up point at the top. Radial offsets from the parent's circle are exaggerated 2.5 times. Half a period after the break-up the fragments are spread 28 degrees along the orbit and 1374 kilometres in altitude, the kicks having carried some to higher apogees and others to lower perigees. After one period the along-track spread has grown to 53 degrees but the whole cloud is only 112 kilometres thick, and the 83 fragments within eight degrees of the break-up point span 35: every fragment's orbit passes through the break-up point, and the cloud pinches there once a period. By 4.5 periods it is 231 degrees long and 863 kilometres thick overall; by 20 it is 352 degrees long, still pinched to 11 kilometres where it began.
Fig. 1 Two hundred and forty fragments thrown from a satellite on a circular orbit 800 kilometres up, with kicks of about 100 metres a second in random directions in the orbital plane, drawn at 0.5, 1, 4.5 and 20 periods of the parent; radial offsets are exaggerated two and a half times. Half a period after the break-up the fragments are spread 28 degrees along the orbit and 1,374 kilometres in altitude. After one period the whole cloud is only 112 kilometres thick, and the fragments near the break-up point span 35. By twenty periods the cloud is 352 degrees long, still pinched to 11 kilometres where it began.

Every orbit contains the point it started from

The pinch is geometry before it is dynamics. Every fragment was at the break-up point at the moment of break-up, so every fragment’s orbit passes through that point, and after one of its own periods each fragment is back there. The orbits are all different ellipses — some larger than the parent’s, some smaller, some tilted — but they share one point, as a bundle of ellipses through a common vertex.

Half a period later the fragments are at the far ends of their different ellipses, and those ends are widely spread: a fragment kicked forward has raised the far side of its orbit, one kicked backward has lowered it, and the cloud there is well over a thousand kilometres deep. A period after the break-up they are all back near the common point, and the cloud has pinched. The pinch is not the fragments being pulled back together; it is the orbits never having separated at that one place.

The picture is in the orbital plane, but the pinch has a second half out of it. A kick perpendicular to the plane tilts a fragment’s orbit about the line joining the break-up point to the Earth’s centre, so every orbital plane contains that line, and the fragments’ paths cross not only at the break-up point but also at the point diametrically opposite it, half an orbit later. The cloud pinches twice a period in the out-of-plane direction: at the break-up point and at the antipodal pinch line, where every fragment’s orbit crosses every other’s. That is where a break-up is most dangerous to anything else in orbit for the first days — the density of fragments there is highest — and it is why a satellite whose orbit happens to pass through a new cloud’s pinch point is at more risk than its altitude alone would suggest.

One component of the kick decides the period

The cloud does not stay pinched in a single clump, because the fragments do not return to the break-up point at the same moment. Each returns after its own period, and the periods differ.

By vis-viva a fragment’s semi-major axis depends on its speed at the break-up point, and its speed there is the vector sum of the parent’s orbital speed and the kick. A kick Δv\Delta v at an angle ϕ\phi to the direction of motion changes the speed to first order by Δvcos⁡ϕ\Delta v\cos\phi — the along-track component — and changes it only at second order through the component across the track. The period depends on the semi-major axis as a3/2a^{3/2}, and the semi-major axis on the speed so that Δa/a=2Δv/v\Delta a/a = 2\Delta v/v for a circular orbit, so

ΔPP=3 Δvcos⁡ϕv.\frac{\Delta P}{P} = 3\,\frac{\Delta v\cos\phi}{v}.

How much a kick changes a fragment's period, by the direction it is thrown. The change in orbital period, in minutes, of a fragment kicked from a circular orbit 800 kilometres up (period 100.9 minutes, speed 7.45 km/s), against the direction of the kick measured from the direction of motion, for kicks of 10, 100, 500 metres a second. Solid: exact, from vis-viva. Dashed: the first-order rule that the fractional change of period is three times the fractional change of the along-track speed. A kick along the motion lengthens the period by 4.2 minutes at 100 m/s; a kick against it shortens it by about as much; a purely radial kick, at 90 degrees, changes it by only 1.6 seconds, because it changes the speed only at second order. The period of a fragment is set by one component of its kick, and it is the component along the orbit.
Fig. 2 The change in orbital period, in minutes, of a fragment kicked from a circular orbit 800 kilometres up (period 100.9 minutes, speed 7.45 kilometres a second), against the direction of the kick, for kicks of 10, 100 and 500 metres a second. Solid: exact, from vis-viva. Dashed: the first-order rule. A 100-metre-a-second kick along the motion lengthens the period by 4.2 minutes; the same kick straight up changes it by 1.6 seconds, because a radial kick changes the speed only at second order.

The factor of three is worth pausing on, because it is large. An along-track kick of 100 metres a second is 1.3 per cent of the orbital speed, and it changes the period by four per cent — four minutes in a hundred. That is why a debris cloud stretches so quickly: a spread of kicks of a hundred metres a second becomes a spread of periods of several minutes, and each period the leading fragments gain several minutes on the trailing ones, which at 7.5 kilometres a second is a couple of thousand kilometres of orbit. It is the same leverage that makes a burn given at speed worth more than the same burn given slowly: the period depends on the energy, and the energy on the square of the speed.

It also explains the counter-intuitive behaviour of orbital rendezvous. A fragment kicked forward, with its speed increased, goes into a larger orbit with a longer period and falls behind the parent’s position; one kicked backward drops into a smaller, faster orbit and gets ahead. To catch up, a spacecraft slows down, and a debris cloud does the same thing in reverse: the fragments thrown forward become the rear of the cloud, and those thrown backward lead it.

The cloud seen from the parent

The same dynamics look different, and in some ways clearer, from a frame that moves with the parent’s orbit — the frame in which rendezvous is planned, with one axis pointing away from the Earth and one along the orbit.

In that frame, and for kicks small compared with the orbital speed, the motion of a fragment is given by the Clohessy–Wiltshire equations, which are linear and can be solved exactly. A fragment kicked straight up — radially — does not drift at all. It moves on a closed ellipse round the parent, twice as long along the track as it is tall, and returns to the parent’s position every period. That relative orbit breathes in and out once a period and goes nowhere, which is the relative-motion statement of the fact that a radial kick leaves the period unchanged.

A fragment kicked along the track drifts. Its orbit has a different period, so in the parent’s frame it traces a series of loops that march steadily away along the track, backward if it was kicked forward and forward if it was kicked backward, by 6π Δv/n6\pi\,\Delta v/n per orbit, where nn is the parent’s orbital frequency. At 800 kilometres, a kick of one metre a second along the track produces a drift of about eighteen kilometres per orbit. The whole along-track stretching of the cloud is that one term, summed over the fragments’ along-track kicks; everything else in the relative motion is periodic and returns to the pinch.

That decomposition is why the stretching is so predictable. A cloud’s shape at any later time is its drift, set by the along-track kicks, plus a breathing, set by the radial and cross-track kicks, and the breathing never accumulates. Every fragment’s relative orbit passes back through the parent’s position — the pinch — or would, if the drift did not carry it along the track first.

The X that every break-up draws

The standard first look at a new break-up is a plot invented by John Gabbard at the North American Aerospace Defense Command in the 1970s: each fragment’s apogee altitude and perigee altitude, plotted against its orbital period.

A Gabbard diagram: the apogee and perigee of every fragment against its period. For 300 fragments of a break-up 800 kilometres up with kicks of about 100 metres a second, spread by half a decade, in random in-plane directions: each fragment's apogee altitude (upper arm) and perigee altitude (lower arm) against its orbital period. The two arms cross at the parent's period, 100.9 minutes, and altitude, 800 km, and form an X — the Gabbard diagram, the standard first look at any break-up. Every perigee lies at or below the break-up altitude and every apogee at or above it, because every orbit passes through the break-up point. Fragments with periods longer than the parent's have their perigee there and rise higher; those with shorter periods have their apogee there and dip lower. 6 fragments were thrown into orbits with perigees below 100 kilometres and re-entered on their first pass. The left arm is where the atmosphere will act first: the fragments on it have the lowest perigees and are the first to be dragged down.
Fig. 3 A Gabbard diagram for three hundred fragments of a break-up 800 kilometres up, with kicks of about 100 metres a second spread by half a decade: each fragment’s apogee (upper arm) and perigee (lower arm) against its period. The arms cross at the parent’s period, 100.9 minutes, and altitude. Every perigee lies at or below the break-up altitude and every apogee at or above it, because every orbit passes through the break-up point; six fragments were thrown into orbits with perigees below 100 kilometres and re-entered on their first pass.

The X is vis-viva again. A fragment with a longer period than the parent’s was kicked forward, gaining speed at the break-up point, so that point is the lowest point of its new orbit: its perigee is at the break-up altitude and its apogee rises with the period. A fragment with a shorter period lost speed there, so the break-up point is its highest point: apogee at the break-up altitude, perigee falling. The horizontal parts of the two arms are the fragments’ shared point; the sloping parts are how far each orbit reaches from it.

A Gabbard diagram therefore identifies the break-up altitude without anyone having seen the break-up: it is where the arms cross and where the flat parts lie. It measures the energy of the event from the spread of the arms. And it predicts the cloud’s future, because the fragments on the lower left, with the lowest perigees, are the ones the atmosphere will act on first. Over months their perigees drag down, their apogees follow, and the left arm of the X is eaten from the bottom.

A Gabbard diagram: the apogee and perigee of every fragment against its period. For 300 fragments of a break-up 480 kilometres up with kicks of about 200 metres a second, spread by half a decade, in random in-plane directions: each fragment's apogee altitude (upper arm) and perigee altitude (lower arm) against its orbital period. The two arms cross at the parent's period, 94.2 minutes, and altitude, 480 km, and form an X — the Gabbard diagram, the standard first look at any break-up. Every perigee lies at or below the break-up altitude and every apogee at or above it, because every orbit passes through the break-up point. Fragments with periods longer than the parent's have their perigee there and rise higher; those with shorter periods have their apogee there and dip lower. 90 fragments were thrown into orbits with perigees below 100 kilometres and re-entered on their first pass. The left arm is where the atmosphere will act first: the fragments on it have the lowest perigees and are the first to be dragged down.
Fig. 4 The same diagram for a break-up 480 kilometres up with kicks of about 200 metres a second — lower and more energetic. The arms cross at 94.2 minutes, and ninety of the three hundred fragments were thrown into orbits with perigees below 100 kilometres and re-entered within one orbit. A low break-up cleans itself up partly on the first pass, because every fragment kicked backward hard enough dips into the atmosphere at the far side of its orbit.

That contrast is the physical basis of a policy argument. The destruction of the Chinese weather satellite Fengyun-1C by a missile in 2007, at about 865 kilometres, produced more than three thousand tracked fragments, most of which are still in orbit, because at that altitude drag takes decades to centuries. The Russian test that destroyed Kosmos 1408 in 2021 was at about 480 kilometres, and its fragments were largely gone within two or three years. The Gabbard diagram of each told, within days, which kind of event it had been.

How long until it is a ring

The cloud stretches along the orbit at a steady rate set by the spread of periods. If the along-track kicks range over ±Δv\pm\Delta v, the periods range over ±3Δv/v\pm 3\Delta v/v of the orbit, and after NN orbits the leading and trailing fragments are separated by 6NΔv/v6N\Delta v/v of a full circle. The cloud closes into a ring when that reaches one: after about v/(6Δv)v/(6\Delta v) orbits.

How quickly a cloud of fragments becomes a ring. The length of orbit occupied by a cloud of fragments — the circle less its largest empty gap, in degrees — against time in orbital periods, sampled half-way between successive returns to the break-up point, for kicks of about 10 and 100 metres a second, 800 kilometres up. The cloud grows along the orbit at a steady rate set by the spread of periods, and it closes into a complete ring after more than 60 periods for 10 m/s and after about 8 periods for 100 m/s. The rule of thumb from vis-viva — a spread of ±Δv along the orbit gives periods differing by ±3Δv/v, so the ring closes after about v/(6Δv) periods — gives 124 and 12. Once the ring has closed, a break-up is no longer a cloud in one place but a hazard everywhere on the orbit, and the next process — the precession of the orbital planes — begins to spread the ring into a shell.
Fig. 5 The length of orbit a cloud occupies — the circle less its largest empty gap — against time in orbital periods, for kicks of about 10 and 100 metres a second, 800 kilometres up. The cloud closes into a complete ring after about 8 periods for 100 metres a second and after more than 60 for 10 metres a second, against the rule of thumb’s 12 and 124. The rule underestimates the speed because the spread of kicks has a tail, and the fastest few fragments set the ends of the cloud.

For a collision or an explosion with typical kicks of a hundred metres a second, a ring forms in about half a day. That is fast compared with anything that can be done about it: by the time a break-up has been detected, tracked and catalogued, its fragments already surround the Earth at that altitude. A break-up is a local event for a few hours and a global hazard at its altitude for as long as the fragments stay up.

The same stretching makes a new cloud hard to catalogue. A tracking radar sees a fragment for a few minutes as it passes overhead, and to add it to a catalogue the fragment has to be recognised on a later pass, which means predicting where it will be. For the first orbits every fragment is near the parent’s path, and the radar sees a swarm it cannot separate; as the cloud stretches the fragments separate along the track, and each can be followed — but only once its period is known well enough to predict its return, which takes several passes. The catalogue of a new break-up therefore fills in over weeks, the fragments with the most distinctive periods first, and the ones kicked least, which stay close to the parent and to each other, last. The fragments that stretch least are the hardest to tell apart, and the early counts of any break-up are lower limits for that reason.

A cloud of fragments that pinches where it was born. 240 fragments thrown from a satellite on a circular orbit 800 kilometres up, with kicks of about 20 metres a second in random directions in the orbital plane, each then following its own Kepler ellipse, drawn at 0.5, 1, 10, 40 orbital periods of the parent, with the Earth's centre marked and the break-up point at the top. Radial offsets from the parent's circle are exaggerated 2.5 times. Half a period after the break-up the fragments are spread 6 degrees along the orbit and 274 kilometres in altitude, the kicks having carried some to higher apogees and others to lower perigees. After one period the along-track spread has grown to 10 degrees but the whole cloud is only 3 kilometres thick, and the 240 fragments within eight degrees of the break-up point span 3: every fragment's orbit passes through the break-up point, and the cloud pinches there once a period. By 10 periods it is 103 degrees long and 65 kilometres thick overall, but 7 at the break-up point; by 40 it is 351 degrees long, still pinched to 8 kilometres where it began.
Fig. 6 A gentle break-up: kicks of about 20 metres a second, 800 kilometres up. Half a period after it the fragments are spread 6 degrees along the orbit and 274 kilometres in altitude; after one period the whole cloud is 3 kilometres thick. By ten periods it is 103 degrees long, and by forty it is a ring, still pinched to 8 kilometres at the break-up point. A slow break-up — the gradual shedding of fragments from an ageing rocket body — takes days rather than hours to surround the Earth, and it pinches just as sharply.

The collision that made the argument concrete

On 10 February 2009 the active communications satellite Iridium 33 and the defunct Russian satellite Kosmos 2251 collided at about 790 kilometres above Siberia, at a relative speed of about 11.7 kilometres a second. It was the first accidental collision between two intact satellites, and the two clouds it produced have been tracked ever since.

Their evolution followed the sequence drawn here. Within hours each cloud was a tight clump at the collision point, pinching there each orbit; within a day each had stretched into a ring; the two rings lay in two different planes, the two satellites’ orbits having been inclined at about 86 and 74 degrees, and their pinch lines crossed at the collision point. Over the following years each ring fanned into a shell as the planes precessed. More than two thousand fragments were catalogued, and a large share are still in orbit, at altitudes where drag works slowly.

The first days after the collision were the most dangerous period for other satellites crossing the pinch points, and the decades after it are the most dangerous period in total, because a shell at 790 kilometres is crossed by everything in low orbit above it on the way up and down. Any object whose orbit passes through the altitude band of a shell has a collision probability per year proportional to the shell’s density, and the shells add. A collision rate needs no collision to be computed; it needs the density, and every break-up raises it. The collision itself was improbable; its products are a permanent part of the environment for everything that shares their altitude.

After the ring: planes and drag

The ring is not the end of the spreading. Two slower processes take over, and each has a clock of its own.

The first is the precession of the orbital planes. The Earth’s equatorial bulge makes the node of an inclined orbit — where it crosses the equator — drift westward or eastward at a rate that depends on the orbit’s size, shape and inclination. Fragments with slightly different semi-major axes and inclinations precess at slightly different rates, so their planes fan out from the parent’s. Over months to a few years the ring, which lies in one plane, becomes a shell: fragments at every longitude of the node, filling the band of latitudes the parent’s inclination allows. The pinch line, where all the planes crossed, dissolves as the planes separate.

The second is drag, and it sorts the fragments. The deceleration from air drag depends on the ratio of a fragment’s area to its mass, which varies over orders of magnitude among the pieces of a broken satellite — a flake of insulating blanket and a chunk of a propellant tank at the same altitude feel very different drag. The high-ratio fragments come down within months; the dense ones stay for decades. The drag depends on an atmospheric density that varies with the solar cycle by a factor of ten at the relevant altitudes, so a break-up at solar maximum clears faster than one at minimum.

The debris environment at any altitude is therefore a superposition of shells of different ages, each the end state of a cloud that pinched, stretched into a ring, fanned into a shell and is slowly being sorted and drained. The rate of collisions it implies is computed from that superposition, and every new break-up adds a layer.

What the figures simplify

The fragments move in the parent’s orbital plane. Out-of-plane kicks tilt the orbits without changing their periods to first order, so they do not change the along-track story; they add the second pinch and, over months, the fanning of planes by precession, which the figures leave to the prose.

The kicks are drawn from a single distribution. Real break-ups have kick distributions that depend on fragment size — small fragments are thrown faster — and on the geometry of the event: an explosion is roughly isotropic, a collision throws most fragments along the relative velocity. The NASA standard break-up model encodes those dependences, and a Gabbard diagram of a real event shows them as asymmetric arms.

The orbits are pure Kepler ellipses. The Earth’s oblateness, drag, the Moon and the Sun are all neglected, which is correct for the first few periods and progressively wrong afterwards; the ring’s closing time is computed before any of them matter much.

And the break-up is instantaneous at a point. A real collision takes milliseconds and throws fragments from an object metres across, so the “point” is a small volume and the pinch has a finite waist even in the ideal case — which the figures’ own waist of a few kilometres, from fragments that have not quite returned, somewhat exceeds.

Still open: what a cloud reveals about the event that made it

A Gabbard diagram of a new break-up is a measurement of the event: the spread of the arms gives the distribution of kick speeds, their asymmetry the direction of the dominant impulse, and the number of fragments on each arm the kind of event. For explosions and collisions of known kinds the relation between the event and the diagram is calibrated by ground tests and by the tracked histories of past break-ups. For break-ups of unknown cause — a satellite that fragments without warning, as several have — the diagram is one of the few pieces of evidence, and reading the event from it is an inverse problem with limited information: the tracked fragments are only those larger than about ten centimetres, which are a small minority of the total and are biased towards the heavier, slower-thrown pieces. Whether the small fragments, which carry most of the collision risk and which radar can barely see, are thrown in the same pattern as the large ones, or faster and more isotropically, decides how the cloud nobody can see or shield against evolves, and it is the part of every break-up that has to be inferred rather than observed.

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FragmentationGabbard diagramNodal precessionOrbital debrisOrbital periodPinch pointSemi-major axisVis-viva equation