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: 20 hours ago
TLE from 20 hours ago
0 CENTAURI-6
1 59451U 24066K 25293.74038872 .00009720 00000-0 73790-3 0 9999
2 59451 45.6058 62.3442 0003886 245.4169 114.6309 15.02497420 84067Epoch: 2025-10-20T17:46Z
TLE epoch observation values (Epoch: 2025-10-20T17:46:09.585Z)
Latitude
-0°
Longitude
126.3659°
Altitude
560.388 km
Speed
7.582 km/s
True Right ascension
04h 09m 22s
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
09:09:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.386 km
Perigee altitude
557.993 km
Semi-major axis
6,938.826 km
Eccentricity
0.00039
Inclination
45.6058°
RAAN
62.3442°
Arg. of periapsis
245.4169°
True anomaly
114.67137°
Mean anomaly
114.6309°
Eccentric anomaly
114.65114°
Mean motion
3.75504 °/min
Orbital period
95.87 mins
BSTAR
0.0007379
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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 | 2025-10-21 14:51:14.217Z | 292.904° NW | 2025-10-21 14:55:14.217Z | 8.858° NNE | 30.922° | 2025-10-21 14:58:14.217Z | 65.263° ENE |
| 6 mins | 2025-10-21 16:33:14.217Z | 303.06° NW | 2025-10-21 16:36:14.217Z | 45.446° ENE | 40.941° | 2025-10-21 16:39:14.217Z | 99.294° ESE |
| 5 mins | 2025-10-21 18:14:14.217Z | 264.266° W | 2025-10-21 18:16:14.217Z | 216.31° SW | 28.727° | 2025-10-21 18:19:14.217Z | 157.512° S |
| 6 mins | 2025-10-22 11:28:14.217Z | 218.221° SW | 2025-10-22 11:31:14.217Z | 121.685° SE | 37.749° | 2025-10-22 11:34:14.217Z | 73.463° E |
| 6 mins | 2025-10-22 13:09:14.217Z | 283.897° WNW | 2025-10-22 13:11:14.217Z | 342.231° N | 36.614° | 2025-10-22 13:15:14.217Z | 60.769° 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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