CENTAURI-8, 62714
Orbit data source: Space-Track
CENTAURI-8, 62714 is a payload satellite owned by Fleet Space (AU) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62714 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
~25 kg wet, ~25 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.222 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-8
1 62714U 25009DK 26171.22915661 .00002932 00000-0 25474-3 0 9996
2 62714 97.7041 251.2989 0003289 123.9306 236.2229 14.97776185 77939Epoch: 2026-06-20T05:29Z
TLE epoch observation values (Epoch: 2026-06-20T05:29:59.131Z)
Latitude
-0.00003°
Longitude
-99.64425°
Altitude
578.093 km
Speed
7.571 km/s
True Right ascension
16h 45m 11s
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
08:41:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.063 km
Perigee altitude
568.492 km
Semi-major axis
6,948.914 km
Eccentricity
0.00033
Inclination
97.7041°
RAAN
251.2989°
Arg. of periapsis
123.9306°
True anomaly
236.19158°
Mean anomaly
236.2229°
Eccentric anomaly
236.20724°
Mean motion
3.74686 °/min
Orbital period
96.08 mins
BSTAR
0.00025474
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Other satellites on launch #9 in the year 2025 (2025-01-14 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-8 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 05:41:34.729Z | 193.23° SSW | 2026-06-21 05:43:34.729Z | 259.173° W | 39.038° | 2026-06-21 05:46:34.729Z | 334.043° NNW |
| 4 mins | 2026-06-21 17:22:34.729Z | 64.526° ENE | 2026-06-21 17:24:34.729Z | 104.099° ESE | 18.965° | 2026-06-21 17:26:34.729Z | 137.259° SSE |
| 5 mins | 2026-06-21 18:57:34.729Z | 329.954° NNW | 2026-06-21 18:59:34.729Z | 282.154° WNW | 25.35° | 2026-06-21 19:02:34.729Z | 231.576° WSW |
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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