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: 19 hours ago
TLE from 19 hours ago
0 AAC-AIS-SAT-1
1 55107U 23001DC 26206.59350890 .00004136 00000-0 40899-3 0 9996
2 55107 97.9186 283.5686 0010390 146.7086 213.4788 14.92416374184011Epoch: 2026-07-25T14:14Z
TLE epoch observation values (Epoch: 2026-07-25T14:14:39.168Z)
Latitude
-0.00006°
Longitude
126.60185°
Altitude
599.484 km
Speed
7.557 km/s
True Right ascension
18h 54m 16s
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
22:11:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.666 km
Perigee altitude
580.192 km
Semi-major axis
6,965.566 km
Eccentricity
0.00104
Inclination
97.9186°
RAAN
283.5686°
Arg. of periapsis
146.7086°
True anomaly
213.41319°
Mean anomaly
213.4788°
Eccentric anomaly
213.44599°
Mean motion
3.73343 °/min
Orbital period
96.43 mins
BSTAR
0.00040899
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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 | 2026-07-26 18:09:51.245Z | 9.313° NNE | 2026-07-26 18:12:51.245Z | 343.951° N | 42.928° | 2026-07-26 18:16:51.245Z | 198.444° SSW |
| 6 mins | 2026-07-27 04:59:51.245Z | 152.588° SSE | 2026-07-27 05:02:51.245Z | 64.336° ENE | 41.965° | 2026-07-27 05:05:51.245Z | 356.331° N |
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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