Showing default

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.

Loading next visibility...
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 (8 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: 1 day ago

TLE from 1 day ago
0 ASTRANIS UTILITYSAT
1 62454U 24252A   25241.92506920 -.00000207  00000-0  00000-0 0  9993
2 62454   8.8105 340.2005 7504874 219.5599  49.6708  1.00411902  2503
Epoch: 2025-08-29T22:12Z
TLE epoch observation values (Epoch: 2025-08-29T22:12:05.978Z)
Latitude
0.00004°
Longitude
28.79195°
Altitude
37,388.691 km
Speed
2.958 km/s
True Right ascension
22h 40m 44s
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
00:01:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
67,368.179 km
Perigee altitude
4,133.584 km
Semi-major axis
42,129.018 km
Eccentricity
0.75049
Inclination
8.8105°
RAAN
340.2005°
Arg. of periapsis
219.5599°
True anomaly
140.33856°
Mean anomaly
49.6708°
Eccentric anomaly
92.62543°
Mean motion
0.251 °/min
Orbital period
1,434.27 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #252 in the year 2024 (2024-12-29 UTC)

Documentation

Showing up to 5 results
|