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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 BUCCANEER MM
1 63245U 25052AM 26206.65810918 .00003108 00000-0 29036-3 0 9993
2 63245 97.6823 96.8765 0005894 85.9041 274.2853 14.94860323 74340Epoch: 2026-07-25T15:47Z
TLE epoch observation values (Epoch: 2026-07-25T15:47:40.633Z)
Latitude
-0.00003°
Longitude
-83.41003°
Altitude
585.55 km
Speed
7.568 km/s
True Right ascension
06h 27m 30s
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
19:21:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.919 km
Perigee altitude
575.717 km
Semi-major axis
6,957.955 km
Eccentricity
0.00059
Inclination
97.6823°
RAAN
96.8765°
Arg. of periapsis
85.9041°
True anomaly
274.21794°
Mean anomaly
274.2853°
Eccentric anomaly
274.25162°
Mean motion
3.73956 °/min
Orbital period
96.27 mins
BSTAR
0.00029036
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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 | 2026-07-26 06:49:28.931Z | 323.09° NNW | 2026-07-26 06:51:28.931Z | 292.273° WNW | 13.824° | 2026-07-26 06:53:28.931Z | 262.622° W |
| 5 mins | 2026-07-26 16:02:28.931Z | 118.646° SE | 2026-07-26 16:04:28.931Z | 81.564° E | 24.233° | 2026-07-26 16:07:28.931Z | 20.046° NNE |
| 4 mins | 2026-07-26 17:38:28.931Z | 230.487° WSW | 2026-07-26 17:40:28.931Z | 269.941° W | 20.356° | 2026-07-26 17:42:28.931Z | 306.03° NW |
| 6 mins | 2026-07-27 05:19:28.931Z | 28.361° NE | 2026-07-27 05:22:28.931Z | 120.146° SE | 38.177° | 2026-07-27 05:25:28.931Z | 175.398° S |
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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