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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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, 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 25318.30000235 .00006645 00000-0 64418-3 0 9993
2 63245 97.7069 208.5992 0003362 189.2162 170.8997 14.93004165 36517Epoch: 2025-11-14T07:12Z
TLE epoch observation values (Epoch: 2025-11-14T07:12:00.203Z)
Latitude
0.00006°
Longitude
46.95286°
Altitude
593.933 km
Speed
7.562 km/s
True Right ascension
13h 54m 23s
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
13:28:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.931 km
Perigee altitude
583.248 km
Semi-major axis
6,963.726 km
Eccentricity
0.00034
Inclination
97.7069°
RAAN
208.5992°
Arg. of periapsis
189.2162°
True anomaly
170.90579°
Mean anomaly
170.8997°
Eccentric anomaly
170.90275°
Mean motion
3.73491 °/min
Orbital period
96.39 mins
BSTAR
0.00064418
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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 | 2025-11-14 16:58:32.122Z | 174.262° S | 2025-11-14 17:01:32.122Z | 226.043° WSW | 43.402° | 2025-11-14 17:05:32.122Z | 343.336° N |
| 6 mins | 2025-11-15 06:17:32.122Z | 344.877° N | 2025-11-15 06:20:32.122Z | 273.054° WNW | 29.346° | 2025-11-15 06:23:32.122Z | 224.286° 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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