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 26082.13082536 .00008363 00000-0 59714-3 0 9997
2 59451 45.6072 343.6950 0001546 322.7723 37.3054 15.04975589107151Epoch: 2026-03-23T03:08Z
TLE epoch observation values (Epoch: 2026-03-23T03:08:23.311Z)
Latitude
0.00006°
Longitude
115.97068°
Altitude
550.794 km
Speed
7.589 km/s
True Right ascension
22h 54m 46s
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
03:04:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
554.145 km
Perigee altitude
552.001 km
Semi-major axis
6,931.21 km
Eccentricity
0.00015
Inclination
45.6072°
RAAN
343.695°
Arg. of periapsis
322.7723°
True anomaly
37.31614°
Mean anomaly
37.3054°
Eccentric anomaly
37.31077°
Mean motion
3.76123 °/min
Orbital period
95.71 mins
BSTAR
0.00059714
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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 | 2026-03-23 22:32:39.008Z | 277.975° WNW | 2026-03-23 22:36:39.008Z | 358.57° N | 33.663° | 2026-03-23 22:39:39.008Z | 57.61° ENE |
| 6 mins | 2026-03-24 00:14:39.008Z | 306.662° NW | 2026-03-24 00:17:39.008Z | 23.808° NE | 32.303° | 2026-03-24 00:20:39.008Z | 76.77° E |
| 6 mins | 2026-03-24 01:55:39.008Z | 291.895° WNW | 2026-03-24 01:57:39.008Z | 248.314° W | 44.512° | 2026-03-24 02:01:39.008Z | 120.087° SE |
| 4 mins | 2026-03-24 19:09:39.008Z | 160.113° S | 2026-03-24 19:10:39.008Z | 140.6° SSE | 18.886° | 2026-03-24 19:13:39.008Z | 92.626° ESE |
| 7 mins | 2026-03-24 20:47:39.008Z | 244.992° WSW | 2026-03-24 20:50:39.008Z | 4.896° NNE | 44.981° | 2026-03-24 20:54:39.008Z | 64.841° 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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