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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 M1
1 43779U 18099X 26124.55969943 .00002164 00000-0 14680-3 0 9997
2 43779 97.4415 168.9483 0013172 175.9362 184.1975 15.07381876405569Epoch: 2026-05-04T13:25Z
TLE epoch observation values (Epoch: 2026-05-04T13:25:58.030Z)
Latitude
-0.0001°
Longitude
105.00937°
Altitude
556.372 km
Speed
7.578 km/s
True Right ascension
11h 15m 47s
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
04:21:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
550.302 km
Perigee altitude
532.074 km
Semi-major axis
6,919.325 km
Eccentricity
0.00132
Inclination
97.4415°
RAAN
168.9483°
Arg. of periapsis
175.9362°
True anomaly
184.18647°
Mean anomaly
184.1975°
Eccentric anomaly
184.19198°
Mean motion
3.77092 °/min
Orbital period
95.47 mins
BSTAR
0.0001468
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-05 02:18:56.342Z | 128.163° SE | 2026-05-05 02:21:56.342Z | 70.936° E | 25.879° | 2026-05-05 02:24:56.342Z | 13.919° NNE |
| 4 mins | 2026-05-05 03:54:56.342Z | 235.306° WSW | 2026-05-05 03:56:56.342Z | 273.654° WNW | 17.781° | 2026-05-05 03:58:56.342Z | 307.104° NW |
| 6 mins | 2026-05-05 15:29:56.342Z | 27.916° NE | 2026-05-05 15:32:56.342Z | 115.897° SE | 37.214° | 2026-05-05 15:35:56.342Z | 174.344° S |
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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