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 25286.96237601 .00007613 00000-0 81667-3 0 9999
2 55107 97.9461 357.6668 0009994 18.6177 341.5403 14.88871377141604Epoch: 2025-10-13T23:05Z
TLE epoch observation values (Epoch: 2025-10-13T23:05:49.287Z)
Latitude
-0.00005°
Longitude
-11.54619°
Altitude
597.876 km
Speed
7.564 km/s
True Right ascension
23h 50m 40s
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
02:54:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.464 km
Perigee altitude
591.519 km
Semi-major axis
6,976.629 km
Eccentricity
0.001
Inclination
97.9461°
RAAN
357.6668°
Arg. of periapsis
18.6177°
True anomaly
341.50399°
Mean anomaly
341.5403°
Eccentric anomaly
341.52215°
Mean motion
3.72456 °/min
Orbital period
96.66 mins
BSTAR
0.00081667
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-14 17:24:03.855Z | 22.864° NE | 2025-10-14 17:28:03.855Z | 102.515° ESE | 38.829° | 2025-10-14 17:32:03.855Z | 177.83° S |
| 5 mins | 2025-10-15 04:17:03.855Z | 121.063° SE | 2025-10-15 04:19:03.855Z | 71.796° E | 30.032° | 2025-10-15 04:22:03.855Z | 10.998° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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