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: 16 hours ago
TLE from 16 hours ago
0 CENTAURI-6
1 59451U 24066K 26036.91626340 .00006971 00000-0 50896-3 0 9994
2 59451 45.6042 219.4188 0001241 160.5618 199.5313 15.04349984100341Epoch: 2026-02-05T21:59Z
TLE epoch observation values (Epoch: 2026-02-05T21:59:25.157Z)
Latitude
-0.00001°
Longitude
113.50234°
Altitude
554.378 km
Speed
7.586 km/s
True Right ascension
14h 37m 40s
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
16:07:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
555.855 km
Perigee altitude
554.134 km
Semi-major axis
6,933.131 km
Eccentricity
0.00012
Inclination
45.6042°
RAAN
219.4188°
Arg. of periapsis
160.5618°
True anomaly
199.52655°
Mean anomaly
199.5313°
Eccentric anomaly
199.52892°
Mean motion
3.75966 °/min
Orbital period
95.75 mins
BSTAR
0.00050896
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-06 14:05:59.551Z | 171.512° S | 2026-02-06 14:07:59.551Z | 138.752° SSE | 16.704° | 2026-02-06 14:09:59.551Z | 105.46° ESE |
| 7 mins | 2026-02-06 15:44:59.551Z | 239.862° WSW | 2026-02-06 15:47:59.551Z | 128.469° SE | 44.751° | 2026-02-06 15:51:59.551Z | 66.063° ENE |
| 6 mins | 2026-02-06 17:25:59.551Z | 290.517° WNW | 2026-02-06 17:28:59.551Z | 10.145° NNE | 31.911° | 2026-02-06 17:31:59.551Z | 60.022° ENE |
| 6 mins | 2026-02-06 19:06:59.551Z | 309.281° NW | 2026-02-06 19:08:59.551Z | 354.295° N | 33.369° | 2026-02-06 19:12:59.551Z | 81.468° E |
| 7 mins | 2026-02-06 20:46:59.551Z | 289.776° WNW | 2026-02-06 20:49:59.551Z | 196.967° SSW | 43.31° | 2026-02-06 20:53:59.551Z | 125.291° SE |
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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