AAC-AIS-SAT-1, 55107
Orbit data source: Space-Track
AAC-AIS-SAT-1, 55107 is a payload satellite owned by AAC ClydeSpace (UK) in SSO that was launched on Tue, 03 Jan 2023 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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55107 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
AAC ClydeSpace
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 AAC-AIS-SAT-1
1 55107U 23001DC 26317.92926464 .00003966 00000-0 38457-3 0 9999
2 55107 97.9088 35.4969 0010088 138.8986 221.2995 14.93227016200622Epoch: 2026-11-13T22:18Z
TLE epoch observation values (Epoch: 2026-11-13T22:18:08.464Z)
Latitude
-0.00003°
Longitude
7.92028°
Altitude
596.204 km
Speed
7.559 km/s
True Right ascension
02h 21m 59s
True Declination
0° 00' 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
23:36:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.929 km
Perigee altitude
577.881 km
Semi-major axis
6,963.042 km
Eccentricity
0.00101
Inclination
97.9088°
RAAN
35.4969°
Arg. of periapsis
138.8986°
True anomaly
221.22328°
Mean anomaly
221.2995°
Eccentric anomaly
221.26138°
Mean motion
3.73546 °/min
Orbital period
96.37 mins
BSTAR
0.00038457
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Other satellites on launch #1 in the year 2023 (2023-01-03 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.AAC-AIS-SAT-1 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-11-14 04:51:37.606Z | 141.008° SSE | 2026-11-14 04:55:37.606Z | 58.776° ENE | 40.143° | 2026-11-14 04:58:37.606Z | 5.38° NNE |
| 6 mins | 2026-11-14 18:10:37.606Z | 15.492° NNE | 2026-11-14 18:13:37.606Z | 137.221° SSE | 80.789° | 2026-11-14 18:16:37.606Z | 190.017° SSW |
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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