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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Edit Public Description
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
0.183 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 CENTAURI-8
1 62714U 25009DK 25286.21386473 .00007399 00000-0 67373-3 0 9990
2 62714 97.7259 4.6787 0000909 219.1285 140.9871 14.95453252 40531Epoch: 2025-10-13T05:07Z
TLE epoch observation values (Epoch: 2025-10-13T05:07:57.912Z)
Latitude
0.00004°
Longitude
-94.33247°
Altitude
584.506 km
Speed
7.568 km/s
True Right ascension
00h 18m 42s
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
18:50:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.611 km
Perigee altitude
577.346 km
Semi-major axis
6,956.116 km
Eccentricity
0.00009
Inclination
97.7259°
RAAN
4.6787°
Arg. of periapsis
219.1285°
True anomaly
140.99366°
Mean anomaly
140.9871°
Eccentric anomaly
140.99038°
Mean motion
3.74105 °/min
Orbital period
96.23 mins
BSTAR
0.00067373
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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 | 2025-10-14 05:20:55.032Z | 165.423° S | 2025-10-14 05:23:55.032Z | 137.847° SSE | 44.889° | 2025-10-14 05:27:55.032Z | 348.341° N |
| 6 mins | 2025-10-14 18:38:55.032Z | 347.699° N | 2025-10-14 18:40:55.032Z | 293.943° NW | 35.507° | 2025-10-14 18:44:55.032Z | 214.133° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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