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, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 M1
1 43779U 18099X 26304.07546114 .00001366 00000-0 92344-4 0 9992
2 43779 97.4230 342.5736 0011197 290.4527 69.5499 15.08132643432616Epoch: 2026-10-31T01:48Z
TLE epoch observation values (Epoch: 2026-10-31T01:48:39.842Z)
Latitude
-0.00003°
Longitude
-83.97879°
Altitude
542.28 km
Speed
7.593 km/s
True Right ascension
22h 50m 17s
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
17:37:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
546.634 km
Perigee altitude
531.144 km
Semi-major axis
6,917.026 km
Eccentricity
0.00112
Inclination
97.423°
RAAN
342.5736°
Arg. of periapsis
290.4527°
True anomaly
69.67018°
Mean anomaly
69.5499°
Eccentric anomaly
69.61003°
Mean motion
3.7728 °/min
Orbital period
95.42 mins
BSTAR
0.000092344
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-01 01:50:28.227Z | 114.853° SE | 2026-11-01 01:53:28.227Z | 64.185° ENE | 19.66° | 2026-11-01 01:55:28.227Z | 29.038° NE |
| 5 mins | 2026-11-01 03:25:28.227Z | 215.289° SW | 2026-11-01 03:27:28.227Z | 258.16° W | 28.264° | 2026-11-01 03:30:28.227Z | 319.204° NNW |
| 5 mins | 2026-11-01 15:01:28.227Z | 46.34° ENE | 2026-11-01 15:03:28.227Z | 94.269° ESE | 32.624° | 2026-11-01 15:06:28.227Z | 157.127° SSE |
| 4 mins | 2026-11-01 16:36:28.227Z | 318.232° NNW | 2026-11-01 16:37:28.227Z | 300.401° NW | 17.368° | 2026-11-01 16:40:28.227Z | 250.613° W |
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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