M1, 43779
Orbit data source: Space-Track
M1, 43779 is a payload satellite owned by RAAF (AU) in SSO that was launched on Mon, 03 Dec 2018 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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43779 intel report (Beta)
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Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
U. NSW
Mission
Non-operational Defense Imaging
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 M1
1 43779U 18099X 26155.09413086 .00002667 00000-0 17915-3 0 9994
2 43779 97.4383 198.4933 0014687 80.6254 279.6634 15.07533485410164Epoch: 2026-06-04T02:15Z
TLE epoch observation values (Epoch: 2026-06-04T02:15:32.906Z)
Latitude
-0.00002°
Longitude
-87.93714°
Altitude
545.12 km
Speed
7.59 km/s
True Right ascension
13h 13m 58s
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
03:07:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
550.885 km
Perigee altitude
530.562 km
Semi-major axis
6,918.861 km
Eccentricity
0.00147
Inclination
97.4383°
RAAN
198.4933°
Arg. of periapsis
80.6254°
True anomaly
279.49744°
Mean anomaly
279.6634°
Eccentric anomaly
279.58042°
Mean motion
3.7713 °/min
Orbital period
95.46 mins
BSTAR
0.00017915
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Other satellites on launch #99 in the year 2018 (2018-12-03 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.M1 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 | 2026-06-12 03:07:46.205Z | 179.199° S | 2026-06-12 03:10:46.205Z | 228.164° WSW | 40.177° | 2026-06-12 03:14:46.205Z | 340.49° N |
| 5 mins | 2026-06-12 16:19:46.205Z | 338.795° N | 2026-06-12 16:21:46.205Z | 288.129° WNW | 29.168° | 2026-06-12 16:24:46.205Z | 226.478° WSW |
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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