Live 3I/ATLAS Tracking Tool

3I/ATLAS - Interstellar Comet Tracker

Interstellar Comet 3I/ATLAS
Live Orbital Tracker

Copyright © 2026 Astrophyzix.org
C/2025 N1 | JPL orbital solution | Keplerian hyperbolic propagation | Real-time

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Live Position
Heliocentric Dist.
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Astronomical Units (AU)
Earth Distance (Delta)
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AU
Heliocentric Speed
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km / s
Est. Visual Mag.
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Apparent magnitude (V)
Right Ascension
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J2000 equatorial
Declination
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J2000 equatorial
Orbit Visualisation
Time offset (days from now): +/-0 d View:
Orbital Elements (JPL SBDB | Solution #51)
ParameterValue
Eccentricity (e)6.141 hyperbolic - interstellar confirmed
Perihelion dist. (q)1.3565 AU between Earth & Mars orbits
Inclination (i)175.11° retrograde, near-ecliptic
Asc. node (Omega)322.16°
Arg. perihelion (omega)128.01°
Perihelion time (T)2025-Oct-29.49 TT JD 2460978.0
Physical / DerivedValue
vinf (hyperbolic excess)~ 57.9 km/s asymptotic interstellar speed
Speed at perihelion~ 68 km/s Solar escape velocity at 1.36 AU
Semi-latus rectum (l)- AU
Origin (kinematics)Milky Way thin/thick disk U,V,W ~ -51,-20,+18 km/s
Earth closest approach2025-Dec-19 1.7976 AU (~269 M km)
Jupiter flyby2026-Mar-16 0.357 AU - gravitational deflection
Comparison: All Known Interstellar Objects
ObjectEccentricityInclinationvinf (km/s)TypeDiscovery
1I/'Oumuamua 1.199122.7°26.3 Inactive | cigar-shaped2017
2I/Borisov 3.35744.1°32.1 Active comet2019
3I/ATLAS * 6.141175.1° 57.9 Active comet | H2O,CO2,CO2025
Speed Context
ISS orbital speed
7.7 km/s
Earth around Sun
29.8 km/s
Voyager 1 (Solar escape)
17.0 km/s
3I/ATLAS perihelion
68 km/s
3I vinf (current, approx)
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Estimated Light Curve (H=11.5, G=10)
Ephemeris - +/-15 Days from Today
Date (UTC) r (AU) Delta Earth (AU) Speed (km/s) Mag (est.) RA (h m s) Dec (° ' ") Elong.
Mission Timeline
2025 Apr 27
Earliest pre-discovery detection - ATLAS photometry, ~4.51 AU from Sun
2025 Jul 01
Official discovery - ATLAS Chile (W68); magnitude 18, 4.51 AU
2025 Jul 02
Designated 3I/ATLAS by Minor Planet Center; third confirmed interstellar object
2025 Aug 06
JWST NIRSpec detects H2O, CO2, CO in coma; carbon-chain depleted
2025 Oct 03
Mars close approach - 0.194 AU; ExoMars TGO imaging
2025 Oct 21
Solar conjunction - comet passes behind Sun (2.59° separation)
2025 Oct 29
PERIHELION - 1.3565 AU from Sun; peak speed 68 km/s; 11:45 UT
2025 Dec 19
Earth closest approach - 1.7976 AU (~269 million km); no impact risk
2026 Mar 16
Jupiter flyby - 0.357 AU; gravitational deflection; +/-600 km 3sigma uncertainty
2026 -> inf
Departure - exits Solar System at ~58 km/s; will not return
Orbital Mechanics Notes

How position is computed in this tracker

> Hyperbolic Kepler equation: M = e|sinh(F) - F solved via Newton-Raphson iteration (converges in <10 steps for e=6.14)

> True anomaly: tan(nu/2) = sqrt((e+1)/(e-1)) | tanh(F/2)

> Heliocentric radius: r = q|(1+e) / (1 + e|cos nu)

> Ecliptic X,Y,Z from nu via Euler rotation: Omega, i, omega (JPL J2000.0 ecliptic)

> Earth position from VSOP87 low-precision L,B,R series truncated to 6 terms

> RA/Dec via ecliptic->equatorial rotation (eps = 23.4393°)

> Magnitude: m = H + 5|log10(r|Delta) + 2.5|log10((1-G)|Phi1 + G|Phi2)

Orbital elements: JPL SBDB solution #51 | Epoch JD 2460978.0 | e=6.141 | q=1.3565 AU | i=175.11° | Omega=322.16° | omega=128.01°

Data source: NASA JPL Small-Body Database | MPC 2025-N12 | Orbital propagation: hyperbolic Kepler + VSOP87

This tracker uses mathematically rigorous Keplerian propagation. For mission-critical applications, use JPL Horizons directly.

3I/ATLAS | C/2025 N1 | Third known interstellar object | Discovered 2025-Jul-01 | No impact risk