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Orbital Eccentricity

Quick answer

Eccentricity measures how stretched an orbit is: 0 is a perfect circle, values approaching 1 are long ellipses, and 1 or more means escape. It is one of the six classical orbital elements, shaping the difference between an orbit's highest and lowest points.

📘 Full definition✓ Reviewed 2026-09-07
Eccentricity (e) is the dimensionless orbital element that describes an orbit's shape. A value of exactly 0 is a circle; values between 0 and 1 are ellipses of increasing elongation; e = 1 is a parabolic escape trajectory and anything higher is hyperbolic — a one-way departure. For a closed orbit, eccentricity links directly to the split between apogee and perigee: the higher the value, the more extreme the difference between the far and near points. Most operational satellites fly near-circular orbits (e below 0.01) because instruments and communication links prefer constant altitude, while deliberately eccentric designs serve special missions: transfer orbits bridge low parking orbits to high destinations, and Molniya-type orbits (e ≈ 0.74) exploit the slow traverse of apogee to loiter over high latitudes. In a TLE, eccentricity appears with an implied leading decimal point — "0006703" means 0.0006703, an almost perfect circle.
Range
0 (circle) to <1 (ellipse)
ISS
0.0001
GEO
0.0002
Molniya
0.74

Understanding Eccentricity

Reading shape from one number

Together with the semi-major axis (size), eccentricity fully fixes an orbit's geometry: perigee radius = a(1−e), apogee radius = a(1+e). A quick mental model: at e = 0.1 the orbit is already visibly oval with apogee about 22% higher than perigee; at e = 0.5 apogee is three times perigee's radius; by e = 0.9 the orbit is a long cigar spending nearly all its period near apogee.

Eccentricity in mission design

Designers choose eccentricity to buy behaviour: transfer orbits use it to reach altitude cheaply; science missions use elongated ellipses to sample plasma environments across radial distance each revolution; and communications designers exploit apogee dwell — the Molniya and Tundra families park their slow apogee segment over a chosen hemisphere, delivering hours of high-elevation coverage per orbit to latitudes that geostationary satellites see poorly.

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Frequently Asked Questions

Almost circular: the ISS and most LEO constellations sit around 0.0001–0.002, geostationary satellites are held below ~0.0005 so they stay put in the sky. Purpose-built eccentric orbits — GTO around 0.73, Molniya around 0.74 — are the striking exceptions.
Kepler's second law: an orbiting body sweeps equal areas in equal times, so it must travel fastest at perigee, the closest point, and slowest at apogee. The more eccentric the orbit, the more dramatic the speed swing — a Molniya satellite crawls through apogee for hours, then whips through perigee in minutes.
Yes — atmospheric drag acting mainly at perigee circularises an orbit by pulling apogee down, while lunar and solar gravity and Earth's asymmetries can pump eccentricity up or down slowly. GEO operators actively manage eccentricity as part of station-keeping.

Sources & References

Definitions are reviewed against primary sources. Last reviewed: 2026-09-07.