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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Edit Public Description
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: 2 days ago
TLE from 2 days ago
0 NUVIEW ALPHA
1 62455U 24252B 25342.43476889 -.00000212 00000-0 00000+0 0 9997
2 62455 0.0519 32.6466 0001707 262.4632 215.7715 1.00266090 1919Epoch: 2025-12-08T10:26Z
TLE epoch observation values (Epoch: 2025-12-08T10:26:04.032Z)
Latitude
0.05013°
Longitude
-83.08597°
Altitude
35,793.506 km
Speed
3.074 km/s
True Right ascension
10h 03m 27s
True Declination
0° 03' 00"
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
00:01:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,796.46 km
Perigee altitude
35,782.064 km
Semi-major axis
42,167.399 km
Eccentricity
0.00017
Inclination
0.0519°
RAAN
32.6466°
Arg. of periapsis
262.4632°
True anomaly
215.76007°
Mean anomaly
215.7715°
Eccentric anomaly
215.76578°
Mean motion
0.25066 °/min
Orbital period
1,436.23 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 | 2025-12-10 01:45:53.505Z | 147.752° SSE | 2025-12-10 08:43:53.505Z | 147.754° SSE | 31.966° | 2025-12-11 01:45:53.505Z | 147.78° 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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