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: 10 hours ago
TLE from 10 hours ago
0 BUCCANEER MM
1 63245U 25052AM 26133.55338528 .00001362 00000-0 13142-3 0 9994
2 63245 97.6907 25.2694 0003619 354.0219 6.0958 14.94479924 63427Epoch: 2026-05-13T13:16Z
TLE epoch observation values (Epoch: 2026-05-13T13:16:52.488Z)
Latitude
0.00003°
Longitude
-45.26106°
Altitude
584.529 km
Speed
7.569 km/s
True Right ascension
01h 41m 04s
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
08:01:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.518 km
Perigee altitude
578.481 km
Semi-major axis
6,959.137 km
Eccentricity
0.00036
Inclination
97.6907°
RAAN
25.2694°
Arg. of periapsis
354.0219°
True anomaly
6.10021°
Mean anomaly
6.0958°
Eccentric anomaly
6.098°
Mean motion
3.73861 °/min
Orbital period
96.29 mins
BSTAR
0.00013142
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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 | 2026-05-14 05:55:37.487Z | 357.853° N | 2026-05-14 05:58:37.487Z | 256.325° W | 38.928° | 2026-05-14 06:01:37.487Z | 208.787° SW |
| 6 mins | 2026-05-14 16:44:37.487Z | 161.242° S | 2026-05-14 16:46:37.487Z | 105.778° ESE | 44.613° | 2026-05-14 16:50:37.487Z | 349.829° N |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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