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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 BUCCANEER MM
1 63245U 25052AM 26091.16822519 .00004537 00000-0 42808-3 0 9990
2 63245 97.6959 343.7396 0005533 105.4320 254.7512 14.94240735 57099Epoch: 2026-04-01T04:02Z
TLE epoch observation values (Epoch: 2026-04-01T04:02:14.656Z)
Latitude
-0°
Longitude
93.6436°
Altitude
588.793 km
Speed
7.565 km/s
True Right ascension
22h 54m 57s
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
18:23:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.594 km
Perigee altitude
577.892 km
Semi-major axis
6,959.88 km
Eccentricity
0.00055
Inclination
97.6959°
RAAN
343.7396°
Arg. of periapsis
105.432°
True anomaly
254.69004°
Mean anomaly
254.7512°
Eccentric anomaly
254.72062°
Mean motion
3.73801 °/min
Orbital period
96.31 mins
BSTAR
0.00042808
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-01 17:02:00.582Z | 184.413° SSW | 2026-04-01 17:04:00.582Z | 233.664° WSW | 40.95° | 2026-04-01 17:08:00.582Z | 339.951° N |
| 4 mins | 2026-04-02 04:45:00.582Z | 66.854° ENE | 2026-04-02 04:46:00.582Z | 84.94° E | 18.038° | 2026-04-02 04:49:00.582Z | 136.208° SSE |
| 5 mins | 2026-04-02 06:20:00.582Z | 334.033° NNW | 2026-04-02 06:22:00.582Z | 286.292° WNW | 27.23° | 2026-04-02 06:25:00.582Z | 230.86° WSW |
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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