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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Edit Public Description
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: 9 hours ago
TLE from 9 hours ago
0 AAC-AIS-SAT-1
1 55107U 23001DC 25345.27798152 .00029182 00000-0 30253-2 0 9991
2 55107 97.9396 56.1956 0010011 172.4964 187.6404 14.89904589150284Epoch: 2025-12-11T06:40Z
TLE epoch observation values (Epoch: 2025-12-11T06:40:17.603Z)
Latitude
-0.0001°
Longitude
-124.11399°
Altitude
608.191 km
Speed
7.551 km/s
True Right ascension
03h 44m 46s
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
13:54:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
602.244 km
Perigee altitude
588.282 km
Semi-major axis
6,973.4 km
Eccentricity
0.001
Inclination
97.9396°
RAAN
56.1956°
Arg. of periapsis
172.4964°
True anomaly
187.62517°
Mean anomaly
187.6404°
Eccentric anomaly
187.63278°
Mean motion
3.72715 °/min
Orbital period
96.59 mins
BSTAR
0.0030253
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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
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-11 16:56:08.880Z | 53.43° ENE | 2025-12-11 16:58:08.880Z | 88.16° E | 20.236° | 2025-12-11 17:01:08.880Z | 140.855° SSE |
| 5 mins | 2025-12-11 18:32:08.880Z | 332.932° NNW | 2025-12-11 18:34:08.880Z | 289.068° WNW | 25.425° | 2025-12-11 18:37:08.880Z | 235.026° WSW |
| 6 mins | 2025-12-12 05:22:08.880Z | 198.064° SSW | 2025-12-12 05:25:08.880Z | 276.444° WNW | 33.472° | 2025-12-12 05:28:08.880Z | 329.77° NNW |
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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