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: 12 hours ago
TLE from 12 hours ago
0 CENTAURI-8
1 62714U 25009DK 25335.18159899 .00006057 00000-0 54329-3 0 9998
2 62714 97.7247 52.9647 0003311 92.3061 267.8539 14.96118683 47851Epoch: 2025-12-01T04:21Z
TLE epoch observation values (Epoch: 2025-12-01T04:21:30.152Z)
Latitude
-0.00008°
Longitude
-82.69571°
Altitude
582.038 km
Speed
7.569 km/s
True Right ascension
03h 31m 51s
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
13:50:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.217 km
Perigee altitude
573.612 km
Semi-major axis
6,954.051 km
Eccentricity
0.00033
Inclination
97.7247°
RAAN
52.9647°
Arg. of periapsis
92.3061°
True anomaly
267.81599°
Mean anomaly
267.8539°
Eccentric anomaly
267.83494°
Mean motion
3.74271 °/min
Orbital period
96.19 mins
BSTAR
0.00054329
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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 | 2025-12-01 17:45:56.581Z | 28.794° NE | 2025-12-01 17:49:56.581Z | 114.593° SE | 32.473° | 2025-12-01 17:52:56.581Z | 167.119° S |
| 4 mins | 2025-12-02 04:35:56.581Z | 104.604° ESE | 2025-12-02 04:37:56.581Z | 60.842° ENE | 22.516° | 2025-12-02 04:39:56.581Z | 24.148° NE |
| 5 mins | 2025-12-02 06:10:56.581Z | 226.394° WSW | 2025-12-02 06:12:56.581Z | 267.834° W | 22.178° | 2025-12-02 06:15:56.581Z | 317.927° NNW |
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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