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: 7 hours ago
TLE from 7 hours ago
0 AAC-AIS-SAT-1
1 55107U 23001DC 26068.82502675 .00007147 00000-0 72543-3 0 9994
2 55107 97.9251 145.1301 0008493 241.0130 119.0237 14.91133831163471Epoch: 2026-03-09T19:48Z
TLE epoch observation values (Epoch: 2026-03-09T19:48:02.311Z)
Latitude
-0.00001°
Longitude
40.60805°
Altitude
600.312 km
Speed
7.558 km/s
True Right ascension
09h 40m 31s
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
06:42:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
597.345 km
Perigee altitude
585.507 km
Semi-major axis
6,969.563 km
Eccentricity
0.00085
Inclination
97.9251°
RAAN
145.1301°
Arg. of periapsis
241.013°
True anomaly
119.10876°
Mean anomaly
119.0237°
Eccentric anomaly
119.06623°
Mean motion
3.73022 °/min
Orbital period
96.51 mins
BSTAR
0.00072543
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-10 04:00:54.847Z | 101.595° ESE | 2026-03-10 04:02:54.847Z | 68.297° E | 17.802° | 2026-03-10 04:04:54.847Z | 34.048° NE |
| 6 mins | 2026-03-10 05:35:54.847Z | 207.236° SW | 2026-03-10 05:37:54.847Z | 248.952° W | 29.492° | 2026-03-10 05:41:54.847Z | 327.506° NNW |
| 5 mins | 2026-03-10 17:19:54.847Z | 47.298° ENE | 2026-03-10 17:21:54.847Z | 93.247° ESE | 28.904° | 2026-03-10 17:24:54.847Z | 156.109° SSE |
| 4 mins | 2026-03-10 18:55:54.847Z | 319.925° NNW | 2026-03-10 18:56:54.847Z | 302.344° NW | 17.975° | 2026-03-10 18:59:54.847Z | 252.072° W |
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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