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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Edit Public Description
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: 16 hours ago
TLE from 16 hours ago
0 BUCCANEER MM
1 63245U 25052AM 26032.49787701 .00003345 00000-0 32087-3 0 9998
2 63245 97.7040 286.2292 0003137 326.6038 33.4983 14.93772769 48335Epoch: 2026-02-01T11:56Z
TLE epoch observation values (Epoch: 2026-02-01T11:56:56.573Z)
Latitude
-0.00011°
Longitude
-24.71316°
Altitude
587.409 km
Speed
7.567 km/s
True Right ascension
19h 04m 55s
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
05:45:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.382 km
Perigee altitude
581.015 km
Semi-major axis
6,961.335 km
Eccentricity
0.00031
Inclination
97.704°
RAAN
286.2292°
Arg. of periapsis
326.6038°
True anomaly
33.51815°
Mean anomaly
33.4983°
Eccentric anomaly
33.50822°
Mean motion
3.73684 °/min
Orbital period
96.34 mins
BSTAR
0.00032087
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-02 04:37:16.085Z | 59.496° ENE | 2026-02-02 04:39:16.085Z | 90.583° ESE | 15.256° | 2026-02-02 04:41:16.085Z | 122.754° SE |
| 6 mins | 2026-02-02 06:12:16.085Z | 348.51° N | 2026-02-02 06:15:16.085Z | 276.859° WNW | 31.658° | 2026-02-02 06:18:16.085Z | 222.586° SW |
| 7 mins | 2026-02-02 17:00:16.085Z | 177.102° S | 2026-02-02 17:04:16.085Z | 293.833° NW | 41.274° | 2026-02-02 17:07:16.085Z | 340.109° 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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