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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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, 0.7 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-7
1 62708U 25009DD 25339.95915794 .00007984 00000-0 71573-3 0 9994
2 62708 97.7268 57.7644 0001970 118.6517 241.4903 14.96041590 48557Epoch: 2025-12-05T23:01Z
TLE epoch observation values (Epoch: 2025-12-05T23:01:11.246Z)
Latitude
0.00006°
Longitude
-2.52624°
Altitude
582.845 km
Speed
7.569 km/s
True Right ascension
03h 51m 03s
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
08:46:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.523 km
Perigee altitude
574.783 km
Semi-major axis
6,954.29 km
Eccentricity
0.0002
Inclination
97.7268°
RAAN
57.7644°
Arg. of periapsis
118.6517°
True anomaly
241.47047°
Mean anomaly
241.4903°
Eccentric anomaly
241.48038°
Mean motion
3.74252 °/min
Orbital period
96.19 mins
BSTAR
0.00071573
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-06 17:16:35.088Z | 62.1° ENE | 2025-12-06 17:18:35.088Z | 97.301° ESE | 17.163° | 2025-12-06 17:20:35.088Z | 130.351° SE |
| 5 mins | 2025-12-06 18:51:35.088Z | 339.353° N | 2025-12-06 18:53:35.088Z | 294.39° NW | 28.418° | 2025-12-06 18:56:35.088Z | 231.118° WSW |
| 6 mins | 2025-12-07 05:39:35.088Z | 189.904° SSW | 2025-12-07 05:41:35.088Z | 249.276° W | 39.782° | 2025-12-07 05:45:35.088Z | 338.579° N |
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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