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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62455 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
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 NUVIEW ALPHA
1 62455U 24252B 26092.19211583 -.00000222 00000-0 00000-0 0 9993
2 62455 0.0654 32.6363 0001884 349.2764 154.6701 1.00271197 3069Epoch: 2026-04-02T04:36Z
TLE epoch observation values (Epoch: 2026-04-02T04:36:38.807Z)
Latitude
0.03384°
Longitude
-83.10031°
Altitude
35,793.471 km
Speed
3.074 km/s
True Right ascension
11h 46m 25s
True Declination
0° 02' 02"
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
13:56:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,795.774 km
Perigee altitude
35,779.886 km
Semi-major axis
42,165.967 km
Eccentricity
0.00019
Inclination
0.0654°
RAAN
32.6363°
Arg. of periapsis
349.2764°
True anomaly
154.67933°
Mean anomaly
154.6701°
Eccentric anomaly
154.67472°
Mean motion
0.25067 °/min
Orbital period
1,436.16 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.NUVIEW ALPHA 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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2026-04-03 08:09:53.896Z | 147.806° SSE | 2026-04-04 02:27:53.896Z | 147.748° SSE | 31.948° | 2026-04-04 08:09:53.896Z | 147.818° SSE |
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62455 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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