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, 1.8 m
Radar Cross Section
0.160 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 BUCCANEER MM
1 63245U 25052AM 26260.53865384 .00001620 00000-0 15301-3 0 9994
2 63245 97.6716 149.6170 0002387 269.6558 90.4389 14.95081345 82392Epoch: 2026-09-17T12:55Z
TLE epoch observation values (Epoch: 2026-09-17T12:55:39.691Z)
Latitude
-0.00007°
Longitude
-40.77282°
Altitude
585.182 km
Speed
7.568 km/s
True Right ascension
09h 58m 28s
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
12:08:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.792 km
Perigee altitude
577.47 km
Semi-major axis
6,957.268 km
Eccentricity
0.00024
Inclination
97.6716°
RAAN
149.617°
Arg. of periapsis
269.6558°
True anomaly
90.46625°
Mean anomaly
90.4389°
Eccentric anomaly
90.45258°
Mean motion
3.74012 °/min
Orbital period
96.25 mins
BSTAR
0.00015301
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-09-18 05:32:50.975Z | 13.235° NNE | 2026-09-18 05:36:50.975Z | 114.49° SE | 85.58° | 2026-09-18 05:40:50.975Z | 191.798° SSW |
| 6 mins | 2026-09-18 16:22:50.975Z | 137.122° SSE | 2026-09-18 16:24:50.975Z | 85.454° E | 47.713° | 2026-09-18 16:28:50.975Z | 0.233° NNE |
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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