UHETSAT, 58466
Orbit data source: Space-Track
UHETSAT, 58466 is a payload satellite owned by SITAEL SpA (IT) in SSO that was launched on Fri, 01 Dec 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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58466 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ITRelated business
Manufacturer
SITAEL SpA
Mission
Operational Commercial Technology
Bus & Motor
S-50, Unknown motor
Mass
70 kg wet, 70 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.360 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 UHETSAT
1 58466U 23185E 25306.49536034 .00007486 00000-0 28094-3 0 9999
2 58466 97.3801 11.1913 0014925 41.4991 318.7379 15.27400593106645Epoch: 2025-11-02T11:53Z
TLE epoch observation values (Epoch: 2025-11-02T11:53:19.133Z)
Latitude
0.00003°
Longitude
150.85131°
Altitude
478.994 km
Speed
7.63 km/s
True Right ascension
00h 44m 45s
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
00:01:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.778 km
Perigee altitude
470.305 km
Semi-major axis
6,858.678 km
Eccentricity
0.00149
Inclination
97.3801°
RAAN
11.1913°
Arg. of periapsis
41.4991°
True anomaly
318.62495°
Mean anomaly
318.7379°
Eccentric anomaly
318.68144°
Mean motion
3.82105 °/min
Orbital period
94.21 mins
BSTAR
0.00028094
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Other satellites on launch #185 in the year 2023 (2023-12-01 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.UHETSAT 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 | 2025-11-03 05:18:49.023Z | 220.334° SW | 2025-11-03 05:20:49.023Z | 256.788° W | 17.886° | 2025-11-03 05:22:49.023Z | 299.847° NW |
| 4 mins | 2025-11-03 16:46:49.023Z | 57.529° ENE | 2025-11-03 16:47:49.023Z | 84.513° E | 26.002° | 2025-11-03 16:50:49.023Z | 155.199° SSE |
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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