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: 6 hours ago
TLE from 6 hours ago
0 CENTAURI-8
1 62714U 25009DK 26122.45475362 .00003777 00000-0 32916-3 0 9993
2 62714 97.7063 203.1819 0000930 34.1400 325.9882 14.97476800 70631Epoch: 2026-05-02T10:54Z
TLE epoch observation values (Epoch: 2026-05-02T10:54:50.712Z)
Latitude
-0.00001°
Longitude
179.09818°
Altitude
577.211 km
Speed
7.572 km/s
True Right ascension
13h 32m 43s
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
00:37:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.351 km
Perigee altitude
571.058 km
Semi-major axis
6,949.842 km
Eccentricity
0.00009
Inclination
97.7063°
RAAN
203.1819°
Arg. of periapsis
34.14°
True anomaly
325.98224°
Mean anomaly
325.9882°
Eccentric anomaly
325.98522°
Mean motion
3.74611 °/min
Orbital period
96.1 mins
BSTAR
0.00032916
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-02 17:53:46.796Z | 25.468° NE | 2026-05-02 17:56:46.796Z | 76.217° E | 36.351° | 2026-05-02 18:00:46.796Z | 174.373° S |
| 5 mins | 2026-05-03 04:42:46.796Z | 112.698° SE | 2026-05-03 04:44:46.796Z | 65.936° ENE | 25.719° | 2026-05-03 04:47:46.796Z | 13.112° NNE |
| 4 mins | 2026-05-03 06:18:46.796Z | 244.322° WSW | 2026-05-03 06:19:46.796Z | 264.465° W | 19.193° | 2026-05-03 06:22:46.796Z | 313.552° NW |
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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