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: 16 hours ago
TLE from 16 hours ago
0 BUCCANEER MM
1 63245U 25052AM 25348.32214331 .00004785 00000-0 46176-3 0 9996
2 63245 97.7071 238.0207 0005766 102.2877 257.8989 14.93321984 40990Epoch: 2025-12-14T07:43Z
TLE epoch observation values (Epoch: 2025-12-14T07:43:53.181Z)
Latitude
0.00004°
Longitude
38.81238°
Altitude
591.476 km
Speed
7.564 km/s
True Right ascension
15h 52m 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
22:20:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.615 km
Perigee altitude
580.586 km
Semi-major axis
6,962.738 km
Eccentricity
0.00058
Inclination
97.7071°
RAAN
238.0207°
Arg. of periapsis
102.2877°
True anomaly
257.8343°
Mean anomaly
257.8989°
Eccentric anomaly
257.8666°
Mean motion
3.73571 °/min
Orbital period
96.37 mins
BSTAR
0.00046176
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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 | 2025-12-15 05:13:02.309Z | 35.246° NE | 2025-12-15 05:16:02.309Z | 104.002° ESE | 32.034° | 2025-12-15 05:19:02.309Z | 163.619° S |
| 5 mins | 2025-12-15 16:03:02.309Z | 110.935° ESE | 2025-12-15 16:05:02.309Z | 72.147° E | 22.575° | 2025-12-15 16:08:02.309Z | 18.778° NNE |
| 4 mins | 2025-12-15 17:39:02.309Z | 231.855° WSW | 2025-12-15 17:40:02.309Z | 252.466° W | 22.324° | 2025-12-15 17:43:02.309Z | 311.537° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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