Orbits

Every orbit one force allows, and the number that picks between them

Circle, ellipse, parabola, hyperbola. A single inverse-square force permits exactly these four, and one number decides which — including whether the body ever comes back.

Apollonius of Perga wrote eight books on the conic sections around 200 BC. He was slicing a cone with a plane and cataloguing the curves that resulted: circle, ellipse, parabola, hyperbola. There is no physics in it anywhere, no force, no motion, and no suggestion that the curves were the shape of anything.

Eighteen hundred and eighty-seven years later, Newton showed that those four curves — all of them, and nothing else — are the complete set of paths a body can follow under an inverse-square attraction. The catalogue was finished long before there was anything to put in it.

Every orbit one force allowsCircle, ellipse, parabola and hyperbola, all sharing a focus and a closest approach. The eccentricity alone decides which one a body is on, and whether it returns.common periapsiscircleellipse, e = 0.5ellipse, e = 0.9parabola, e = 1hyperbola, e = 1.5e < 1 returnse ≥ 1 never does
Fig. 1 The four conics, sharing a focus and a closest approach. Only the eccentricity differs between them, and it alone decides whether the body returns.

One family, one parameter

Every one of these curves obeys the same equation,

r(ν)=p1+ecosν,r(\nu) = \frac{p}{1 + e\cos\nu},

with rr the distance from the focus, ν\nu the angle from the closest approach, pp a scale, and ee the eccentricity. That single formula produces all four, and the transitions between them are entirely in the denominator.

At e=0e = 0 the cosine term vanishes and rr is constant: a circle. For 0<e<10 < e < 1 the denominator stays positive at every angle, so rr is finite everywhere and the curve closes: an ellipse. At e=1e = 1 the denominator reaches zero at ν=180°\nu = 180°, so rr runs to infinity there and the curve never closes: a parabola. For e>1e > 1 the denominator hits zero earlier, at cosν=1/e\cos\nu = -1/e, and beyond that angle the formula returns nothing at all: a hyperbola, whose asymptotes are exactly those forbidden directions.

That last case is the one worth pausing on. The angles at which the equation has no solution are not a defect of the formula. They are the directions the body came in from and leaves along, and they are as much part of the trajectory as the curve is.

Every orbit one force allowsCircle, ellipse, parabola and hyperbola, all sharing a focus and a closest approach. The eccentricity alone decides which one a body is on, and whether it returns.common periapsisellipse, e = 0.4ellipse, e = 0.7ellipse, e = 0.95e < 1 returnse ≥ 1 never does
Fig. 2 Three ellipses that differ only in eccentricity. As ee approaches 1 the far end runs away without limit while the near end stays put — the parabola is the limit of this process, not a different kind of thing.

The apoapsis distance is p/(1e)p/(1-e), which grows without bound as e1e \to 1. So the parabola is what an ellipse becomes when its far end is pushed to infinity, and the hyperbola is what happens when it is pushed past. Nothing discontinuous occurs anywhere in the family, which is a good deal less obvious than the four names suggest.

What the number really is

The eccentricity looks geometric and is really an energy.

The total energy per unit mass of an orbiting body is kinetic plus potential:

ε=v22GMr,\varepsilon = \frac{v^2}{2} - \frac{GM}{r},

and it is conserved. Its sign has an immediate meaning. Negative means the body is bound — it has less kinetic energy than it would need to climb out of the well, and it will come back. Positive means it is unbound and leaving for good. Zero is the boundary.

The eccentricity is related to it by

e=1+2εh2(GM)2,e = \sqrt{1 + \frac{2\varepsilon h^2}{(GM)^2}},

where hh is the specific angular momentum. Every feature of the family follows from the sign of ε\varepsilon under the square root: negative energy gives e<1e < 1, zero gives exactly 1, positive gives more than 1.

So the four shapes are three energy regimes and a boundary case, and the boundary is a set of measure zero. No real orbit is a parabola. A comet whose energy is within a part in 101210^{12} of zero is on an extremely long ellipse or a barely hyperbolic path, and the difference is measurable; a parabola requires exactly zero, which nothing has. Parabolic orbits appear constantly in the literature as approximations for long-period comets, and every one of them is a convenience.

Speed against distance, for orbits of the same periodOrbital speed against distance from the primary. Every orbit with the same semi-major axis follows the same curve; the eccentricity decides only which stretch of it the body uses.00.511.50123distance from the primary (a = 1)e = 0e = 0.4e = 0.8circular speed at r = a
Fig. 3 Speed against distance for bound orbits sharing a semi-major axis. The whole curve is the vis-viva relation, and the term that fixes it — the one in 1/a1/a — is the energy in disguise.

The vis-viva relation makes the energy visible. Written as v2=GM(2/r1/a)v^2 = GM(2/r - 1/a), the second term carries the energy: for a bound orbit aa is positive and the term is a subtraction, for a hyperbola aa is negative and the term becomes an addition, and for a parabola it is absent entirely, leaving v2=2GM/rv^2 = 2GM/r, which is the escape speed exactly.

A negative semi-major axis is a strange object and it is the right bookkeeping. A hyperbolic orbit has no far end, so “half the long axis” has nothing to measure, and the quantity that appears in the equations is the one that keeps the algebra working.

The visitors that settled it

For two centuries every known object in the solar system was on a bound orbit. Comets appeared on paths so elongated that their eccentricities were indistinguishable from 1, and the question of whether any of them came from outside was unanswerable with the available precision.

Then in October 2017 a small object was found moving at 26 km/s relative to the Sun while still beyond the Earth’s orbit — far too fast to be bound. Its eccentricity came out at 1.20, which is not marginally above 1 and not a measurement error. ʻOumuamua came in from interstellar space, swung round the Sun on a hyperbola, and left. Borisov followed in 2019 at e=3.36e = 3.36, which is emphatically unbound.

Those two objects are the observational proof that the upper half of the conic family is occupied. Before them it was a mathematical possibility with no known instance; the theory had predicted an entire branch of the curve family that nothing had ever been seen on.

An orbit at eccentricity 0.95An orbit of eccentricity 0.95. The primary sits at a focus, offset from the centre by 0.95 of the semi-major axis, and the closest and furthest points differ by a factor of 39.00.empty focusrperiapsisapoapsis
Fig. 4 An orbit at eccentricity 0.95 — a long-period comet. The body spends almost all of its time in the far half, and the entire close approach that makes it visible occupies a vanishing fraction of the period.

Why exactly these curves

The result that an inverse-square force gives conics is not obvious, and the reason is a hidden conserved quantity.

Any central force conserves energy and angular momentum. That is enough to confine the motion to a plane and to fix the range of distances, but not enough to make the orbit close: in general the direction of closest approach drifts round, and the path is a rosette that fills an annulus and never repeats.

The inverse square conserves one thing more — a vector that points from the focus toward periapsis and has a length equal to the eccentricity. It is called the Laplace–Runge–Lenz vector, and its constancy is exactly the statement that the direction of closest approach does not move. That is what makes the orbit close, and it is the extra symmetry that singles out the inverse square from every other exponent.

Bertrand’s theorem makes the uniqueness precise: of all central forces, exactly two produce closed orbits for every bound trajectory — the inverse square and the linear spring. Both were known to Newton, both are conic sections, and the difference between them is where the centre of attraction sits. For the spring the force pulls toward the centre of the ellipse; for gravity, toward a focus. Same curve, two different laws, distinguished by which point is occupied — which is the geometric content of Kepler’s first law restated as a claim about force.

The conserved vector also gives the cleanest test of whether gravity is exactly inverse-square. If it is not, the vector is not conserved, and the orbit precesses. Mercury’s orbit precesses by 574 arcseconds per century, of which 531 come from the other planets. The remaining 43 are not Newtonian, and they are among the most consequential leftovers in the history of physics.

The family used deliberately

Interplanetary navigation lives in this family and moves between its branches on purpose.

Circular and escape speedOrbital and escape speed against distance, in units of the circular speed at the surface. The escape curve is the circular one multiplied by the square root of two, at every distance without exception.2468101200.511.5distance, in body radiiescape speedcircular speedthe surfacea high orbitgeostationarythe gap is always a factor of √2
Fig. 5 Circular and escape speed against distance. The gap between them is the whole of the family: below the lower curve nothing stays up, between them the orbit is an ellipse, on the upper curve it is parabolic, and above it hyperbolic.

A spacecraft leaving Earth is on a hyperbola with respect to the Earth and an ellipse with respect to the Sun, simultaneously, and the two descriptions are stitched together at the edge of Earth’s gravitational influence. That patched-conic method — treat the trajectory as a sequence of two-body conics, each valid in its own region — is how every mission from Mariner to New Horizons was planned. It is an approximation with no rigorous justification and it works to within a course correction.

A gravity assist is a hyperbolic pass, and the turn angle it delivers is set entirely by the eccentricity of that hyperbola. The tighter the pass, the lower the eccentricity, the sharper the turn, and the more speed the manoeuvre extracts.

Moving between branches on purpose

The family is not just a classification. A spacecraft changes which member of it is on, deliberately, several times per mission.

A Hohmann transfer, 2.6 to 1 in radiusTwo circular orbits and the ellipse that touches both. The first burn raises the far point to the outer orbit; the second, half an orbit later, circularises. The costs are computed from the vis-viva relation.burn 1: +0.202burn 2: +0.158total 0.360 — and no way to spend lesscoast: half an ellipse, 1.21 of an inner-orbit yearspeeds in units of the inner circular speed
Fig. 6 A transfer between two circular orbits. Every stage is a different conic: a circle, then an ellipse, then a larger circle — and each transition is a burn that changes the energy at a fixed position.

Each burn moves the vehicle to a different conic through the same point, because a burn changes velocity and not position. Add enough energy at once and the conic becomes a hyperbola, which is what leaving means. The whole of trajectory design is a sequence of hops between members of this one family.

A flyby does the same thing without a burn. Passing a planet puts the spacecraft on a hyperbola with respect to that planet while leaving it on an ellipse with respect to the Sun — two conics at once, in two frames, both exact.

Where the model stops

Two bodies. The conics are exact only for two point masses alone. With three, no closed-form solution exists at all, and the trajectory is not a conic and not any other named curve.

Point masses. Extended bodies deviate, and close binaries deviate a lot.

No drag, no thrust, no radiation pressure. A comet outgassing near perihelion is being thrust, and the resulting non-gravitational acceleration is large enough to have made ʻOumuamua’s orbit briefly controversial.

Newtonian gravity. Near a compact object, orbits precess and eventually decay by radiating gravitational waves — a possibility the conic family has no room for at all, since it conserves energy exactly.

And a limitation of the picture. All these figures are drawn in a plane and face-on, which no observer ever sees. A conic in space needs three more numbers to say how the plane is tilted and turned, and those three are where the practical difficulty of orbit determination actually lies. Knowing that a newly-found object is on a hyperbola is easy; knowing where it will be next month is not.

The ladder from here

Later rungs: the derivation of the orbit equation from Newton’s laws. The Laplace–Runge–Lenz vector and the hidden symmetry behind it. Bertrand’s theorem. Hyperbolic anomaly, and Kepler’s equation for unbound orbits. The patched-conic method and spheres of influence. Interstellar objects, and what their arrival rate implies about how many there are. Radial trajectories, the degenerate case with zero angular momentum, which the family contains and no figure shows. And the orbits of general relativity, where the conics acquire a precession and, close in, stop closing at all.

Apollonius called the curves ellipse, parabola and hyperbola — deficient, exact and excessive — after how a certain area compared with a reference rectangle. The names describe an arithmetic comparison in a geometry problem, and they now describe the energy budget of everything that moves under gravity.