PROTOMETHEE, 58321
Orbit data source: Space-Track
PROTOMETHEE, 58321 is a payload satellite owned by Promethee (FR) in SSO that was launched on Sat, 11 Nov 2023 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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58321 intel report (Beta)
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Identifier
Orbit
Country
FRRelated business
Manufacturer
NanoAvionics
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
30 kg wet, ~30 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 PROTOMETHEE
1 58321U 23174BT 26079.76742422 .00004592 00000-0 15923-3 0 9997
2 58321 97.3814 158.6809 0009496 115.8605 244.3616 15.30278335131440Epoch: 2026-03-20T18:25Z
TLE epoch observation values (Epoch: 2026-03-20T18:25:05.452Z)
Latitude
-0.00003°
Longitude
64.11042°
Altitude
480.908 km
Speed
7.623 km/s
True Right ascension
10h 34m 43s
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
08:04:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
478.437 km
Perigee altitude
465.427 km
Semi-major axis
6,850.069 km
Eccentricity
0.00095
Inclination
97.3814°
RAAN
158.6809°
Arg. of periapsis
115.8605°
True anomaly
244.26355°
Mean anomaly
244.3616°
Eccentric anomaly
244.31257°
Mean motion
3.82825 °/min
Orbital period
94.04 mins
BSTAR
0.00015923
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Other satellites on launch #174 in the year 2023 (2023-11-11 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.PROTOMETHEE 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 | 2026-03-22 05:04:40.499Z | 155.023° SSE | 2026-03-22 05:07:40.499Z | 35.426° NE | 40.183° | 2026-03-22 05:10:40.499Z | 354.53° N |
| 5 mins | 2026-03-22 18:04:40.499Z | 12.92° NNE | 2026-03-22 18:06:40.499Z | 187.494° SSW | 43.829° | 2026-03-22 18:09:40.499Z | 192.405° SSW |
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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