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, 0.7 m
Radar Cross Section
0.222 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 4 hours ago
TLE from 4 hours ago
0 CENTAURI-7
1 62708U 25009DD 26126.50369677 .00004269 00000-0 37086-3 0 9997
2 62708 97.7084 207.3137 0001970 79.9864 280.1580 14.97532796 71222Epoch: 2026-05-06T12:05Z
TLE epoch observation values (Epoch: 2026-05-06T12:05:19.400Z)
Latitude
-0.00008°
Longitude
161.61963°
Altitude
577.332 km
Speed
7.572 km/s
True Right ascension
13h 49m 15s
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
00:12:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.9 km
Perigee altitude
570.162 km
Semi-major axis
6,949.668 km
Eccentricity
0.0002
Inclination
97.7084°
RAAN
207.3137°
Arg. of periapsis
79.9864°
True anomaly
280.13578°
Mean anomaly
280.158°
Eccentric anomaly
280.14689°
Mean motion
3.74625 °/min
Orbital period
96.1 mins
BSTAR
0.00037086
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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 | 2026-05-06 17:28:59.699Z | 46.537° ENE | 2026-05-06 17:31:59.699Z | 104.163° ESE | 22.355° | 2026-05-06 17:33:59.699Z | 141.168° SSE |
| 5 mins | 2026-05-06 19:04:59.699Z | 327.305° NNW | 2026-05-06 19:06:59.699Z | 285.027° WNW | 22.109° | 2026-05-06 19:09:59.699Z | 237.003° WSW |
| 6 mins | 2026-05-07 05:51:59.699Z | 203.411° SW | 2026-05-07 05:53:59.699Z | 253.025° W | 32.714° | 2026-05-07 05:57:59.699Z | 332.167° 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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