Mission Control/CNEOS BOLIDE DOSSIER: CNEOS-FB-06
GEMMA ENGINE: LOCAL SERVER BOX [ACTIVE]Launch in 3D CesiumJS Globe
JPL SSD CNEOS ATMOSPHERIC BOLIDE AIRBURSThttp://127.0.0.1:11434/v1 • meteors-gemma:latest

Tasman Basin Atmospheric Fragmentation (cneos-fb-06)

At 2026-08-24 02:51:11 UTC, U.S. Government infrasound and geostationary lightning mapper sensors recorded bolide cneos-fb-06 entering Earth's atmosphere above (-33.70°, 151.20°). Traveling along an ECEF 3D velocity vector of (vx=11.5, vy=-15.2, vz=-7.4) km/s (speed 20.50 km/s), hydrodynamic stagnation ram pressure peaked at 15.94 MPa at 27.8 km altitude, triggering catastrophic fragmentation with 1.34e+13 Joules radiated optical energy and 3.20 kilotons TNT total acoustic-kinetic yield.

Impact Yield
3.20 kt
Kilotons TNT Eq.
Airburst Altitude
27.8 km
Ram: 15.94 MPa
Radiated Energy
1.34e+13 J
Optical Bolide Flash
Entry Velocity
20.50 km/s
3D Vector Solved

Signed Geodetic Coordinates & 3D Velocity Vector

ECEF (vx, vy, vz)
UTC Event Timestamp2026-08-24 02:51:11
Signed Geodetic Latitude / Longitude-33.700°, 151.200°
Peak Energy Deposition Altitude (altKm)27.80 km MSL
3D Velocity Components (vx, vy, vz)[11.50, -15.20, -7.40] km/s
Peak Stagnation Ram Pressure15.94 MPa

Atmospheric Bolide Frequently Asked Questions

Where did CNEOS bolide cneos-fb-06 detonate in the atmosphere?

Bolide cneos-fb-06 reached peak aerodynamic breakup at 27.8 km altitude over signed coordinates (-33.70°, 151.20°) on 2026-08-24 02:51:11 UTC.

How is the 3D entry vector (11.5, -15.2, -7.4) km/s used in CesiumJS?

Meteors.ai converts the Earth-Centered Earth-Fixed (ECEF) velocity vector into a 3D atmospheric entry ray on our NASA GIBS WMTS globe, illustrating the exact entry azimuth and airburst altitude (27.8 km).

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CNEOS Bolide CNEOS-FB-06 (3.2 kt TNT) — 3D Vector & Airburst Dossier | Meteors.ai Space Network