MACSAT, 58024
Orbit data source: Space-Track
MACSAT, 58024 is a payload satellite owned by OQ Tech (LU) in SSO that was launched on Mon, 09 Oct 2023 UTC via a VEGA launch vehicle from the French Guiana (FRGUI). 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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58024 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / LUXERelated business
Manufacturer
NanoAvionics
Mission
Operational Commercial 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, 0.3 m
Radar Cross Section
0.098 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 MACSAT
1 58024U 23155J 25307.66794779 .00005311 00000-0 26369-3 0 9996
2 58024 97.5996 23.6090 0003932 118.6403 241.5226 15.18119913114081Epoch: 2025-11-03T16:01Z
TLE epoch observation values (Epoch: 2025-11-03T16:01:50.689Z)
Latitude
-0.00004°
Longitude
99.98178°
Altitude
515.898 km
Speed
7.605 km/s
True Right ascension
01h 34m 26s
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
03:53:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.208 km
Perigee altitude
505.792 km
Semi-major axis
6,886.637 km
Eccentricity
0.00039
Inclination
97.5996°
RAAN
23.609°
Arg. of periapsis
118.6403°
True anomaly
241.483°
Mean anomaly
241.5226°
Eccentric anomaly
241.5028°
Mean motion
3.7978 °/min
Orbital period
94.79 mins
BSTAR
0.00026369
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Other satellites on launch #155 in the year 2023 (2023-10-09 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.MACSAT 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 | 2025-11-04 17:54:04.754Z | 19.436° NNE | 2025-11-04 17:57:04.754Z | 73.362° E | 41.375° | 2025-11-04 18:00:04.754Z | 180.762° SSW |
| 5 mins | 2025-11-05 04:34:04.754Z | 115.356° SE | 2025-11-05 04:36:04.754Z | 69.459° E | 23.893° | 2025-11-05 04:39:04.754Z | 13.746° NNE |
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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