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, 0.8 m
Radar Cross Section
0.222 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 CENTAURI-8
1 62714U 25009DK 26278.23247882 .00002753 00000-0 23593-3 0 9999
2 62714 97.6974 356.8833 0003347 125.2574 234.8962 14.98353318 93958Epoch: 2026-10-05T05:34Z
TLE epoch observation values (Epoch: 2026-10-05T05:34:46.170Z)
Latitude
-0.00001°
Longitude
-100.7234°
Altitude
576.375 km
Speed
7.572 km/s
True Right ascension
23h 47m 31s
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
19:23:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
571.316 km
Perigee altitude
566.666 km
Semi-major axis
6,947.128 km
Eccentricity
0.00033
Inclination
97.6974°
RAAN
356.8833°
Arg. of periapsis
125.2574°
True anomaly
234.86483°
Mean anomaly
234.8962°
Eccentric anomaly
234.88051°
Mean motion
3.74831 °/min
Orbital period
96.04 mins
BSTAR
0.00023593
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-06 05:45:02.898Z | 191.363° SSW | 2026-10-06 05:48:02.898Z | 275.616° WNW | 47.769° | 2026-10-06 05:51:02.898Z | 333.245° NNW |
| 5 mins | 2026-10-06 17:26:02.898Z | 55.739° ENE | 2026-10-06 17:28:02.898Z | 94.171° ESE | 22.489° | 2026-10-06 17:31:02.898Z | 145.304° SSE |
| 5 mins | 2026-10-06 19:01:02.898Z | 334.309° NNW | 2026-10-06 19:03:02.898Z | 293.916° NW | 26.216° | 2026-10-06 19:06:02.898Z | 237.897° 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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