ASTRANIS UTILITYSAT, 62454
Orbit data source: Space-Track
ASTRANIS UTILITYSAT, 62454 is a UK payload satellite in HEO that was launched on Sun, 29 Dec 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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62454 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
Astranis
Mission
Operational Commercial Communications
Bus & Motor
MICROGEO, EP
Mass
400 kg wet, 400 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 22 Pan, 5.0 m
Radar Cross Section
41.175 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 ASTRANIS UTILITYSAT
1 62454U 24252A 26191.01587836 -.00000023 00000-0 00000-0 0 9999
2 62454 8.9946 326.3176 7581812 255.9951 17.7292 1.00284966 5655Epoch: 2026-07-10T00:22Z
TLE epoch observation values (Epoch: 2026-07-10T00:22:51.890Z)
Latitude
0.00008°
Longitude
33.03102°
Altitude
15,732.26 km
Speed
5.157 km/s
True Right ascension
21h 46m 47s
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
10:45:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
67,755.034 km
Perigee altitude
3,818.079 km
Semi-major axis
42,164.693 km
Eccentricity
0.75818
Inclination
8.9946°
RAAN
326.3176°
Arg. of periapsis
255.9951°
True anomaly
105.41272°
Mean anomaly
17.7292°
Eccentric anomaly
51.92652°
Mean motion
0.25068 °/min
Orbital period
1,436.09 mins
BSTAR
0
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Other satellites on launch #252 in the year 2024 (2024-12-29 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.ASTRANIS UTILITYSAT 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. |
|---|---|---|---|---|---|---|---|
| 22 mins | 2026-07-14 22:14:39.424Z | 205.546° SW | 2026-07-14 22:14:39.424Z | 205.546° SW | 23.789° | 2026-07-14 22:36:39.424Z | 161.729° S |
| 813 mins | 2026-07-15 08:41:39.424Z | 91.748° ESE | 2026-07-15 15:16:39.424Z | 179.157° S | 39.679° | 2026-07-15 22:14:39.424Z | 198.983° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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