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NUVIEW ALPHA, 62455

Orbit data source: Space-Track

NUVIEW ALPHA, 62455 is a UK payload satellite in GEO 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
62455, 2024-252B
Orbit
GEO
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

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 NUVIEW ALPHA
1 62455U 24252B   26286.36796021 -.00000216  00000-0  00000-0 0  9995
2 62455   0.0672  39.5722 0000255 235.9559 155.7847  1.00271851  5004
Epoch: 2026-10-13T08:49Z
TLE epoch observation values (Epoch: 2026-10-13T08:49:51.762Z)
Latitude
0.02556°
Longitude
-83.10953°
Altitude
35,787.041 km
Speed
3.075 km/s
True Right ascension
04h 45m 09s
True Declination
0° 01' 32"
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
16:50:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,788.722 km
Perigee altitude
35,786.572 km
Semi-major axis
42,165.784 km
Eccentricity
0.00003
Inclination
0.0672°
RAAN
39.5722°
Arg. of periapsis
235.9559°
True anomaly
155.7859°
Mean anomaly
155.7847°
Eccentric anomaly
155.7853°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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Other satellites on launch #252 in the year 2024 (2024-12-29 UTC)

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