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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Edit Public Description
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: 19 hours ago
TLE from 19 hours ago
0 M1
1 43779U 18099X 25260.08643690 .00003515 00000-0 24789-3 0 9995
2 43779 97.4813 306.6219 0012319 245.1681 114.8265 15.05554650371019Epoch: 2025-09-17T02:04Z
TLE epoch observation values (Epoch: 2025-09-17T02:04:28.148Z)
Latitude
-0.00004°
Longitude
-80.76281°
Altitude
556.465 km
Speed
7.581 km/s
True Right ascension
20h 26m 29s
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
13:32:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
555.323 km
Perigee altitude
538.261 km
Semi-major axis
6,924.929 km
Eccentricity
0.00123
Inclination
97.4813°
RAAN
306.6219°
Arg. of periapsis
245.1681°
True anomaly
114.95454°
Mean anomaly
114.8265°
Eccentric anomaly
114.89053°
Mean motion
3.76635 °/min
Orbital period
95.58 mins
BSTAR
0.00024789
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-18 02:09:33.078Z | 102.187° ESE | 2025-09-18 02:11:33.078Z | 70.979° E | 15.13° | 2025-09-18 02:13:33.078Z | 37.366° NE |
| 6 mins | 2025-09-18 03:43:33.078Z | 200.681° SSW | 2025-09-18 03:46:33.078Z | 275.349° WNW | 30.958° | 2025-09-18 03:49:33.078Z | 328.998° NNW |
| 4 mins | 2025-09-18 15:21:33.078Z | 58.069° ENE | 2025-09-18 15:23:33.078Z | 104.138° ESE | 23.027° | 2025-09-18 15:25:33.078Z | 142.87° SSE |
| 4 mins | 2025-09-18 16:56:33.078Z | 318.137° NNW | 2025-09-18 16:57:33.078Z | 297.283° NW | 20.313° | 2025-09-18 17:00:33.078Z | 243.185° 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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