CENTAURI-6, 59451
Orbit data source: Space-Track
CENTAURI-6, 59451 is a payload satellite owned by Fleet Space (AU) in LEO that was launched on Sun, 07 Apr 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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59451 intel report (Beta)
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Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
Terran Orbital
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
0.222 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 CENTAURI-6
1 59451U 24066K 26218.74653949 .00002692 00000-0 19720-3 0 9999
2 59451 45.6074 350.3593 0001752 296.7332 63.3372 15.06246021127749Epoch: 2026-08-06T17:55Z
TLE epoch observation values (Epoch: 2026-08-06T17:55:01.011Z)
Latitude
-0.00008°
Longitude
126.32284°
Altitude
547.205 km
Speed
7.59 km/s
True Right ascension
23h 21m 26s
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
14:36:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
550.39 km
Perigee altitude
547.963 km
Semi-major axis
6,927.314 km
Eccentricity
0.00018
Inclination
45.6074°
RAAN
350.3593°
Arg. of periapsis
296.7332°
True anomaly
63.35514°
Mean anomaly
63.3372°
Eccentric anomaly
63.34617°
Mean motion
3.7644 °/min
Orbital period
95.63 mins
BSTAR
0.0001972
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Other satellites on launch #66 in the year 2024 (2024-04-07 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-6 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 | 2026-08-08 11:29:22.252Z | 221.041° SW | 2026-08-08 11:33:22.252Z | 135.158° SSE | 36.485° | 2026-08-08 11:36:22.252Z | 76.086° E |
| 6 mins | 2026-08-08 13:10:22.252Z | 273.062° WNW | 2026-08-08 13:13:22.252Z | 345.146° N | 37.347° | 2026-08-08 13:16:22.252Z | 56.266° ENE |
| 6 mins | 2026-08-08 14:51:22.252Z | 303.246° NW | 2026-08-08 14:54:22.252Z | 14.533° NNE | 30.759° | 2026-08-08 14:57:22.252Z | 69.168° E |
| 6 mins | 2026-08-08 16:32:22.252Z | 301.555° NW | 2026-08-08 16:34:22.252Z | 345.912° N | 43.045° | 2026-08-08 16:38:22.252Z | 107.21° ESE |
| 5 mins | 2026-08-08 18:12:22.252Z | 263.302° W | 2026-08-08 18:14:22.252Z | 224.324° SW | 23.588° | 2026-08-08 18:17:22.252Z | 167.586° S |
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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