BUCCANEER MM, 63245
Orbit data source: Space-Track
BUCCANEER MM, 63245 is an Australian payload satellite in SSO that was launched on Sat, 15 Mar 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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63245 intel report (Beta)
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Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
U. NSW
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Ant, 0.2 m
Radar Cross Section
0.160 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 BUCCANEER MM
1 63245U 25052AM 26223.72667630 .00001315 00000-0 12566-3 0 9999
2 63245 97.6787 113.5885 0005207 45.2293 314.9351 14.94934981 76894Epoch: 2026-08-11T17:26Z
TLE epoch observation values (Epoch: 2026-08-11T17:26:24.832Z)
Latitude
0.00003°
Longitude
-108.20579°
Altitude
583.063 km
Speed
7.57 km/s
True Right ascension
07h 34m 21s
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
14:30:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.209 km
Perigee altitude
575.963 km
Semi-major axis
6,957.723 km
Eccentricity
0.00052
Inclination
97.6787°
RAAN
113.5885°
Arg. of periapsis
45.2293°
True anomaly
314.89284°
Mean anomaly
314.9351°
Eccentric anomaly
314.91397°
Mean motion
3.73975 °/min
Orbital period
96.26 mins
BSTAR
0.00012566
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Other satellites on launch #52 in the year 2025 (2025-03-15 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.BUCCANEER MM 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 | 2026-08-12 05:15:21.453Z | 26.746° NE | 2026-08-12 05:18:21.453Z | 84.167° E | 36.646° | 2026-08-12 05:22:21.453Z | 174.261° S |
| 5 mins | 2026-08-12 16:05:21.453Z | 112.04° ESE | 2026-08-12 16:07:21.453Z | 64.627° ENE | 25.876° | 2026-08-12 16:10:21.453Z | 12.731° NNE |
| 4 mins | 2026-08-12 17:41:21.453Z | 242.37° WSW | 2026-08-12 17:42:21.453Z | 262.073° W | 19.185° | 2026-08-12 17:45:21.453Z | 312.236° NW |
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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