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: 9 hours ago
TLE from 9 hours ago
0 BUCCANEER MM
1 63245U 25052AM 25304.29175972 .00005274 00000-0 51485-3 0 9994
2 63245 97.7075 194.8751 0002563 256.5054 103.5880 14.92824952 34429Epoch: 2025-10-31T07:00Z
TLE epoch observation values (Epoch: 2025-10-31T07:00:08.039Z)
Latitude
-0.00004°
Longitude
50.00332°
Altitude
592.597 km
Speed
7.563 km/s
True Right ascension
12h 59m 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
11:43:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.932 km
Perigee altitude
584.362 km
Semi-major axis
6,964.284 km
Eccentricity
0.00026
Inclination
97.7075°
RAAN
194.8751°
Arg. of periapsis
256.5054°
True anomaly
103.61655°
Mean anomaly
103.588°
Eccentric anomaly
103.60227°
Mean motion
3.73447 °/min
Orbital period
96.4 mins
BSTAR
0.00051485
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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 | 2025-10-31 16:46:17.267Z | 162.43° S | 2025-10-31 16:50:17.267Z | 37.568° NE | 44.276° | 2025-10-31 16:53:17.267Z | 350.937° N |
| 6 mins | 2025-11-01 06:06:17.267Z | 350.548° N | 2025-11-01 06:08:17.267Z | 300.47° NW | 36.532° | 2025-11-01 06:12:17.267Z | 213.062° 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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