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: 11 hours ago
TLE from 11 hours ago
0 BUCCANEER MM
1 63245U 25052AM 25256.96149074 .00002092 00000-0 21009-3 0 9992
2 63245 97.7127 148.5149 0005753 64.2502 295.9310 14.92326021 27363Epoch: 2025-09-13T23:04Z
TLE epoch observation values (Epoch: 2025-09-13T23:04:32.799Z)
Latitude
-0.00009°
Longitude
169.19091°
Altitude
591.977 km
Speed
7.565 km/s
True Right ascension
09h 54m 03s
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
02:41:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.708 km
Perigee altitude
583.694 km
Semi-major axis
6,965.838 km
Eccentricity
0.00058
Inclination
97.7127°
RAAN
148.5149°
Arg. of periapsis
64.2502°
True anomaly
295.87169°
Mean anomaly
295.931°
Eccentric anomaly
295.90135°
Mean motion
3.73322 °/min
Orbital period
96.43 mins
BSTAR
0.00021009
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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 | 2025-09-14 16:53:35.675Z | 167.942° S | 2025-09-14 16:57:35.675Z | 325.452° NNW | 44.605° | 2025-09-14 17:00:35.675Z | 346.455° N |
| 6 mins | 2025-09-15 06:13:35.675Z | 347.673° N | 2025-09-15 06:15:35.675Z | 305.879° NW | 32.368° | 2025-09-15 06:19:35.675Z | 219.343° SW |
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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