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: 6 hours ago
TLE from 6 hours ago
0 AAC-AIS-SAT-1
1 55107U 23001DC 26115.52111200 .00004649 00000-0 46803-3 0 9998
2 55107 97.9203 192.0362 0010879 95.2318 265.0142 14.91636175170434Epoch: 2026-04-25T12:30Z
TLE epoch observation values (Epoch: 2026-04-25T12:30:24.076Z)
Latitude
-0.00004°
Longitude
150.8976°
Altitude
596.538 km
Speed
7.561 km/s
True Right ascension
12h 48m 08s
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
01:46:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
597.44 km
Perigee altitude
582.279 km
Semi-major axis
6,967.997 km
Eccentricity
0.00109
Inclination
97.9203°
RAAN
192.0362°
Arg. of periapsis
95.2318°
True anomaly
264.89002°
Mean anomaly
265.0142°
Eccentric anomaly
264.95211°
Mean motion
3.73148 °/min
Orbital period
96.48 mins
BSTAR
0.00046803
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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 | 2026-04-26 04:44:24.447Z | 144.837° SSE | 2026-04-26 04:47:24.447Z | 75.355° E | 37.82° | 2026-04-26 04:51:24.447Z | 358.231° N |
| 7 mins | 2026-04-26 18:03:24.447Z | 8.685° NNE | 2026-04-26 18:06:24.447Z | 295.956° NW | 44.389° | 2026-04-26 18:10:24.447Z | 198.321° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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