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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Edit Public Description
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, 1.0 m
Radar Cross Section
0.183 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 CENTAURI-6
1 59451U 24066K 25344.18964182 .00006022 00000-0 45295-3 0 9997
2 59451 45.6038 160.0101 0002500 187.5594 172.5251 15.03425138 91653Epoch: 2025-12-10T04:33Z
TLE epoch observation values (Epoch: 2025-12-10T04:33:05.053Z)
Latitude
-0.00005°
Longitude
12.57546°
Altitude
558.128 km
Speed
7.583 km/s
True Right ascension
10h 40m 02s
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
16:58:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
559.57 km
Perigee altitude
556.102 km
Semi-major axis
6,935.973 km
Eccentricity
0.00025
Inclination
45.6038°
RAAN
160.0101°
Arg. of periapsis
187.5594°
True anomaly
172.52883°
Mean anomaly
172.5251°
Eccentric anomaly
172.52696°
Mean motion
3.75735 °/min
Orbital period
95.81 mins
BSTAR
0.00045295
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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 | 2025-12-10 19:18:18.112Z | 300.674° NW | 2025-12-10 19:22:18.112Z | 32.994° NE | 35.34° | 2025-12-10 19:25:18.112Z | 85.762° E |
| 6 mins | 2025-12-10 21:00:18.112Z | 278.973° WNW | 2025-12-10 21:02:18.112Z | 216.476° SW | 39.634° | 2025-12-10 21:06:18.112Z | 133.726° SE |
| 6 mins | 2025-12-11 14:13:18.112Z | 200.413° SSW | 2025-12-11 14:16:18.112Z | 142.551° SSE | 27.513° | 2025-12-11 14:19:18.112Z | 85.395° E |
| 6 mins | 2025-12-11 15:54:18.112Z | 264.266° W | 2025-12-11 15:56:18.112Z | 320.682° NNW | 41.841° | 2025-12-11 16:00:18.112Z | 61.437° ENE |
| 5 mins | 2025-12-11 17:35:18.112Z | 306.195° NW | 2025-12-11 17:37:18.112Z | 357.303° N | 31.006° | 2025-12-11 17:40:18.112Z | 60.883° ENE |
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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