M2-A, 47967 (Decayed)
Orbit data source: Space-Track
M2-A, 47967 was an Australian payload satellite in LEO that was launched on Mon, 22 Mar 2021 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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47967 intel report (Beta)
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Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
U. NSW
Mission
Decayed Amateur Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan + 1 Ant, 0.4 m
Radar Cross Section
0.112 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 M2-A
1 47967U 21023C 25090.98843926 .05289429 10267-4 15128-2 0 9994
2 47967 44.9707 114.4192 0004584 54.2067 28.9373 16.26595675223363Epoch: 2025-03-31T23:43Z
TLE epoch observation values (Epoch: 2025-03-31T23:43:21.152Z)
Latitude
44.72961°
Longitude
9.36434°
Altitude
202.719 km
Speed
7.793 km/s
True Right ascension
12h 59m 11s
True Declination
44° 32' 35"
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
21:30:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
206.404 km
Perigee altitude
200.37 km
Semi-major axis
6,581.524 km
Eccentricity
0.00046
Inclination
44.9707°
RAAN
114.4192°
Arg. of periapsis
54.2067°
True anomaly
28.96273°
Mean anomaly
28.9373°
Eccentric anomaly
28.95001°
Mean motion
4.06493 °/min
Orbital period
88.56 mins
BSTAR
0.0015128
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Other satellites on launch #23 in the year 2021 (2021-03-22 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.M2-A Visibility
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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. |
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| This satellite is decayed. |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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