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Comet 3I/ATLAS The third known interstellar object, on its hyperbolic orbit

Comets · interstellar

3I/ATLAS, from elsewhere

Discovered on 1 July 2025 by the ATLAS survey in Chile, 3I/ATLAS is the third object known to come from another star system, after ʻOumuamua (2017) and Borisov (2019). Its open orbit (e > 1) takes it through the solar system only once.

Date
—
Distance from the Sun
—
Distance from the Earth
—
Perihelion
2025-10-29
1,350 au from the Sun
Eccentricity
6.12
e > 1: hyperbolic orbit, not bound to the Sun
Speed at infinity
58.0 km/s
≈ 208 692 km/h relative to the Sun
Inclination
175 °
retrograde orbit, close to the plane of the planets
Interstellar comet 3I/ATLAS (C/2025 N1): JPL orbit solution · NASA/JPL, public domain (cite JPL SSD/CNEOS) · 10/23/26 Interstellar comet 3I/ATLAS: heliocentric trajectory (JPL Horizons) · NASA/JPL, public domain (cite JPL SSD/CNEOS) · 10/23/26

Heliocentric trajectory from JPL Horizons (4-day steps); planets from the JPL approximate Keplerian elements. Sizes and tail illustrative.

A comet from another star system

Spotted by the ATLAS telescope at Río Hurtado (Chile) on 1 July 2025, the comet immediately showed an orbit impossible for a solar-system body: its eccentricity exceeds 6, and its speed far from the Sun, close to 58 km/s, is that of an object arriving from interstellar space.

It passed about 0.2 au from Mars in early October 2025, reached perihelion at the end of October, 1.36 au from the Sun, then moved away, passing 1.8 au from the Earth in December and close to Jupiter in March 2026. Like ʻOumuamua and Borisov before it, it will not return.

The elements and trajectory shown here are those of the latest JPL orbit solution; they are updated at each import.

Computed approaches
BodyDateMinimum distance
Sun (perihelion)2025-10-291,350 au
Mercury2025-10-081,162 au (174 M km)
Venus2025-11-030,650 au (97 M km)
Earth2025-12-191,798 au (269 M km)
Mars2025-10-030,195 au (29 M km)
Jupiter2026-03-160,358 au (54 M km)
Orbital elements (JPL SBDB)
Eccentricity e6.12 ± 4.4e-05
Perihelion distance q1.35 au ± 4.1e-06
Inclination i175 deg ± 7.7e-05
Longitude of the ascending node Ω323 deg ± 0.00052
Argument of perihelion ω129 deg ± 0.00053
Perihelion time (JD TDB)2460977.942 TDB ± 0.00018
Semi-major axis a-0.264 au ± 1.8e-06
comet total magnitude slope7.5
comet total magnitude11.8
Solution55 · arc 2025-10-03 → 2026-10-16, 117 observations
Method and sources

The trajectory is imported weekly from the JPL Horizons API (heliocentric vectors, ecliptic J2000) and the orbital elements daily from the JPL Small-Body Database. Distances to the planets are computed here with Standish’s approximate elements.

Reading these data
An active comet feels non-gravitational forces (outgassing): successive orbit solutions change slightly. The M1 and K1 magnitudes describe an average brightness, not a size.
SOURCES OF THIS PAGE
Interstellar comet 3I/ATLAS (C/2025 N1): JPL orbit solution
NASA/JPL Small-Body Database, 3I/ATLAS (C/2025 N1), osculating orbital elements and photometric parameters. · source page ↗
Licence : NASA/JPL, public domain (cite JPL SSD/CNEOS) · retrieved on Oct 23, 2026 · SHA-256 3f47134b36cd…
Interstellar comet 3I/ATLAS: heliocentric trajectory (JPL Horizons)
NASA/JPL Horizons, heliocentric ecliptic J2000 position vectors of 3I/ATLAS. · source page ↗
Licence : NASA/JPL, public domain (cite JPL SSD/CNEOS) · retrieved on Oct 23, 2026 · SHA-256 75b09d7319a0…