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: 23 hours ago
TLE from 23 hours ago
0 M1
1 43779U 18099X 25310.58954421 .00004809 00000-0 33283-3 0 9999
2 43779 97.4729 355.5859 0015253 77.6959 282.5975 15.06046933378619Epoch: 2025-11-06T14:08Z
TLE epoch observation values (Epoch: 2025-11-06T14:08:56.619Z)
Latitude
-0.00005°
Longitude
97.30431°
Altitude
549.074 km
Speed
7.589 km/s
True Right ascension
23h 42m 20s
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
08:55:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
555.841 km
Perigee altitude
534.721 km
Semi-major axis
6,923.418 km
Eccentricity
0.00153
Inclination
97.4729°
RAAN
355.5859°
Arg. of periapsis
77.6959°
True anomaly
282.42685°
Mean anomaly
282.5975°
Eccentric anomaly
282.51218°
Mean motion
3.76758 °/min
Orbital period
95.55 mins
BSTAR
0.00033283
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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 | 2025-11-07 16:13:28.525Z | 2.687° NNE | 2025-11-07 16:16:28.525Z | 294.017° NW | 41.199° | 2025-11-07 16:19:28.525Z | 207.352° SW |
| 5 mins | 2025-11-08 02:58:28.525Z | 145.323° SSE | 2025-11-08 03:00:28.525Z | 58.18° ENE | 40.786° | 2025-11-08 03:03:28.525Z | 357.143° N |
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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