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ASTRANIS UTILITYSAT, 62454

Orbit data source: Space-Track

ASTRANIS UTILITYSAT, 62454 is a payload satellite owned by Astranis (UK) 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 (11 months 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: 12 hours ago

TLE from 12 hours ago
0 ASTRANIS UTILITYSAT
1 62454U 24252A   25343.56631287 -.00000289  00000-0  00000+0 0  9990
2 62454   8.9327 335.1316 7511341 232.1256  34.1206  1.00314732  3524
Epoch: 2025-12-09T13:35Z
TLE epoch observation values (Epoch: 2025-12-09T13:35:29.431Z)
Latitude
-0.00002°
Longitude
52.85004°
Altitude
27,753.844 km
Speed
3.728 km/s
True Right ascension
22h 21m 05s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
00:01:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
67,443.063 km
Perigee altitude
4,113.109 km
Semi-major axis
42,156.223 km
Eccentricity
0.75113
Inclination
8.9327°
RAAN
335.1316°
Arg. of periapsis
232.1256°
True anomaly
128.36421°
Mean anomaly
34.1206°
Eccentric anomaly
75.852°
Mean motion
0.25076 °/min
Orbital period
1,435.66 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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