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: 19 hours ago
TLE from 19 hours ago
0 CENTAURI-6
1 59451U 24066K 26140.06839805 .00003341 00000-0 24534-3 0 9996
2 59451 45.6073 41.3383 0001784 288.0246 72.0444 15.05525117115889Epoch: 2026-05-20T01:38Z
TLE epoch observation values (Epoch: 2026-05-20T01:38:29.591Z)
Latitude
0.00003°
Longitude
138.98178°
Altitude
549.579 km
Speed
7.589 km/s
True Right ascension
02h 45m 21s
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
05:32:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
552.623 km
Perigee altitude
550.151 km
Semi-major axis
6,929.524 km
Eccentricity
0.00018
Inclination
45.6073°
RAAN
41.3383°
Arg. of periapsis
288.0246°
True anomaly
72.06385°
Mean anomaly
72.0444°
Eccentric anomaly
72.05412°
Mean motion
3.7626 °/min
Orbital period
95.68 mins
BSTAR
0.00024534
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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 | 2026-05-20 20:57:41.708Z | 237.446° WSW | 2026-05-20 21:01:41.708Z | 111.923° ESE | 43.772° | 2026-05-20 21:04:41.708Z | 67.835° E |
| 6 mins | 2026-05-20 22:39:41.708Z | 291.717° WNW | 2026-05-20 22:41:41.708Z | 340.953° N | 33.089° | 2026-05-20 22:45:41.708Z | 61.186° ENE |
| 5 mins | 2026-05-21 00:20:41.708Z | 313.565° NW | 2026-05-21 00:22:41.708Z | 8.617° NNE | 33.329° | 2026-05-21 00:25:41.708Z | 75.454° E |
| 6 mins | 2026-05-21 02:00:41.708Z | 290.715° WNW | 2026-05-21 02:02:41.708Z | 267.356° W | 42.255° | 2026-05-21 02:06:41.708Z | 122.933° SE |
| 5 mins | 2026-05-21 19:13:41.708Z | 176.792° S | 2026-05-21 19:15:41.708Z | 139.659° SSE | 20.112° | 2026-05-21 19:18:41.708Z | 90.974° ESE |
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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