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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BUCCANEER MM radio frequencies
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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, 1.8 m
Radar Cross Section
0.160 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 BUCCANEER MM
1 63245U 25052AM 25261.25271543 .00003210 00000-0 31921-3 0 9994
2 63245 97.7131 152.7180 0005687 54.7871 305.3880 14.92352786 28006Epoch: 2025-09-18T06:03Z
TLE epoch observation values (Epoch: 2025-09-18T06:03:54.613Z)
Latitude
0°
Longitude
64.32347°
Altitude
591.351 km
Speed
7.566 km/s
True Right ascension
10h 10m 52s
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
07:11:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.579 km
Perigee altitude
583.656 km
Semi-major axis
6,965.755 km
Eccentricity
0.00057
Inclination
97.7131°
RAAN
152.718°
Arg. of periapsis
54.7871°
True anomaly
305.33485°
Mean anomaly
305.388°
Eccentric anomaly
305.36143°
Mean motion
3.73328 °/min
Orbital period
96.43 mins
BSTAR
0.00031921
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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 | 2025-09-18 15:52:55.451Z | 101.622° ESE | 2025-09-18 15:54:55.451Z | 67.76° E | 17.582° | 2025-09-18 15:56:55.451Z | 33.498° NE |
| 6 mins | 2025-09-18 17:27:55.451Z | 209.019° SW | 2025-09-18 17:29:55.451Z | 252.356° W | 29.035° | 2025-09-18 17:33:55.451Z | 328.199° NNW |
| 6 mins | 2025-09-19 05:10:55.451Z | 42.711° NE | 2025-09-19 05:12:55.451Z | 84.207° E | 29.061° | 2025-09-19 05:16:55.451Z | 162.686° S |
| 4 mins | 2025-09-19 06:46:55.451Z | 322.424° NNW | 2025-09-19 06:48:55.451Z | 286.837° WNW | 17.466° | 2025-09-19 06:50:55.451Z | 254.967° W |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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