CENTAURI-9, 69924
Orbit data source: Space-Track
CENTAURI-9, 69924 is a payload satellite owned by Fleet Space (AU) in SSO that was launched on Tue, 07 Jul 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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69924 intel report (Beta)
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Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
Terran Orbital
Mission
Operational spacecraft
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
~25 kg wet, ~25 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
BOX+2 PAN, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 CENTAURI-9
1 69924U 26156BH 26237.16101283 .00000824 00000-0 86436-4 0 9997
2 69924 97.7469 136.8264 0008295 2.2789 357.8466 14.92179932 7289Epoch: 2026-08-25T03:51Z
TLE epoch observation values (Epoch: 2026-08-25T03:51:51.508Z)
Latitude
-0.00006°
Longitude
105.42945°
Altitude
588.404 km
Speed
7.569 km/s
True Right ascension
09h 07m 18s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
05:46:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.936 km
Perigee altitude
582.379 km
Semi-major axis
6,966.295 km
Eccentricity
0.00083
Inclination
97.7469°
RAAN
136.8264°
Arg. of periapsis
2.2789°
True anomaly
357.84302°
Mean anomaly
357.8466°
Eccentric anomaly
357.84481°
Mean motion
3.73285 °/min
Orbital period
96.44 mins
BSTAR
0.000086436
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Other satellites on launch #156 in the year 2026 (2026-07-07 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.CENTAURI-9 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-25 16:51:51.486Z | 138.453° SSE | 2026-08-25 16:55:51.486Z | 62.06° ENE | 30.613° | 2026-08-25 16:58:51.486Z | 8.022° NNE |
| 4 mins | 2026-08-25 18:29:51.486Z | 243.348° WSW | 2026-08-25 18:30:51.486Z | 260.073° W | 15.724° | 2026-08-25 18:33:51.486Z | 306.841° NW |
| 6 mins | 2026-08-26 06:11:51.486Z | 18.308° NNE | 2026-08-26 06:13:51.486Z | 43.49° NE | 42.565° | 2026-08-26 06:17:51.486Z | 187.952° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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