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: 17 hours ago
TLE from 17 hours ago
0 CENTAURI-8
1 62714U 25009DK 26074.20647420 .00004269 00000-0 37327-3 0 9996
2 62714 97.7084 155.5938 0002694 103.0184 257.1339 14.97275858 63411Epoch: 2026-03-15T04:57Z
TLE epoch observation values (Epoch: 2026-03-15T04:57:19.370Z)
Latitude
-0.00003°
Longitude
-91.55353°
Altitude
578.786 km
Speed
7.571 km/s
True Right ascension
10h 22m 22s
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
02:10:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.199 km
Perigee altitude
570.454 km
Semi-major axis
6,950.464 km
Eccentricity
0.00027
Inclination
97.7084°
RAAN
155.5938°
Arg. of periapsis
103.0184°
True anomaly
257.10381°
Mean anomaly
257.1339°
Eccentric anomaly
257.11885°
Mean motion
3.74561 °/min
Orbital period
96.11 mins
BSTAR
0.00037327
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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 | 2026-03-16 05:08:25.624Z | 152.865° SSE | 2026-03-16 05:11:25.624Z | 100.707° ESE | 40.334° | 2026-03-16 05:15:25.624Z | 355.96° N |
| 6 mins | 2026-03-16 18:25:25.624Z | 2.334° NNE | 2026-03-16 18:27:25.624Z | 324.82° NNW | 41.279° | 2026-03-16 18:31:25.624Z | 203.158° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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