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: 16 hours ago
TLE from 16 hours ago
0 CENTAURI-7
1 62708U 25009DD 26307.24925867 .00002547 00000-0 21746-3 0 9991
2 62708 97.7018 25.7557 0003032 95.9809 264.1759 14.98565534 98287Epoch: 2026-11-03T05:58Z
TLE epoch observation values (Epoch: 2026-11-03T05:58:55.949Z)
Latitude
-0.00002°
Longitude
-106.49205°
Altitude
574.595 km
Speed
7.573 km/s
True Right ascension
01h 43m 01s
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
18:08:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.441 km
Perigee altitude
566.229 km
Semi-major axis
6,946.472 km
Eccentricity
0.0003
Inclination
97.7018°
RAAN
25.7557°
Arg. of periapsis
95.9809°
True anomaly
264.14134°
Mean anomaly
264.1759°
Eccentric anomaly
264.15862°
Mean motion
3.74884 °/min
Orbital period
96.03 mins
BSTAR
0.00021746
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-04 04:33:35.044Z | 118.654° SE | 2026-11-04 04:36:35.044Z | 67.8° E | 22.718° | 2026-11-04 04:39:35.044Z | 18.148° NNE |
| 5 mins | 2026-11-04 06:09:35.044Z | 221.977° SW | 2026-11-04 06:11:35.044Z | 264.785° W | 26.288° | 2026-11-04 06:14:35.044Z | 318.597° NNW |
| 6 mins | 2026-11-04 17:49:35.044Z | 40.054° NE | 2026-11-04 17:51:35.044Z | 89.642° E | 40.38° | 2026-11-04 17:55:35.044Z | 169.393° S |
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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