CENTAURI-7, 62708
Orbit data source: Space-Track
CENTAURI-7, 62708 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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62708 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: 8 hours ago
TLE from 8 hours ago
0 CENTAURI-7
1 62708U 25009DD 26262.44138867 .00003162 00000-0 27044-3 0 9990
2 62708 97.7036 341.5228 0001469 112.6074 247.5304 14.98324518 91575Epoch: 2026-09-19T10:35Z
TLE epoch observation values (Epoch: 2026-09-19T10:35:35.981Z)
Latitude
0°
Longitude
-175.727°
Altitude
575.516 km
Speed
7.573 km/s
True Right ascension
22h 46m 05s
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
11:24:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.101 km
Perigee altitude
568.06 km
Semi-major axis
6,947.218 km
Eccentricity
0.00015
Inclination
97.7036°
RAAN
341.5228°
Arg. of periapsis
112.6074°
True anomaly
247.51485°
Mean anomaly
247.5304°
Eccentric anomaly
247.52262°
Mean motion
3.74824 °/min
Orbital period
96.05 mins
BSTAR
0.00027044
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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-7 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-19 19:10:00.205Z | 339.49° N | 2026-09-19 19:13:00.205Z | 289.519° WNW | 21.264° | 2026-09-19 19:15:00.205Z | 253.097° W |
| 5 mins | 2026-09-20 05:58:00.205Z | 210.997° SW | 2026-09-20 06:00:00.205Z | 261.473° W | 35.375° | 2026-09-20 06:03:00.205Z | 324.02° NNW |
| 5 mins | 2026-09-20 17:38:00.205Z | 45.382° ENE | 2026-09-20 17:40:00.205Z | 85.278° E | 29.625° | 2026-09-20 17:43:00.205Z | 150.645° SSE |
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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