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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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Identifier
62454, 2024-252A
Orbit
HEO
Country
Flag of UKUK
Related business
Manufacturer
Astranis
Mission
Operational Commercial Communications
Bus & Motor
MICROGEO, EP
Mass
400 kg wet, 400 kg dry
Launch date (UTC)
2024-12-29 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 22 Pan, 5.0 m
Radar Cross Section
41.175 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 ASTRANIS UTILITYSAT
1 62454U 24252A   26239.86872826 -.00000057  00000-0  00000+0 0  9997
2 62454   9.1485 324.9615 7546027 261.0817  15.6326  1.00296967  6140
Epoch: 2026-08-27T20:50Z
TLE epoch observation values (Epoch: 2026-08-27T20:50:58.121Z)
Latitude
0.00023°
Longitude
36.42959°
Altitude
14,473.505 km
Speed
5.364 km/s
True Right ascension
21h 41m 05s
True Declination
0° 00' 01"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
22:20:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
67,598.119 km
Perigee altitude
3,968.122 km
Semi-major axis
42,161.257 km
Eccentricity
0.7546
Inclination
9.1485°
RAAN
324.9615°
Arg. of periapsis
261.0817°
True anomaly
99.30077°
Mean anomaly
15.6326°
Eccentric anomaly
47.51875°
Mean motion
0.25071 °/min
Orbital period
1,435.92 mins
BSTAR
0
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Other satellites on launch #252 in the year 2024 (2024-12-29 UTC)

Documentation

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