AAC-AIS-SAT2, 56996
Orbit data source: Space-Track
AAC-AIS-SAT2, 56996 is a payload satellite owned by AAC ClydeSpace (UK) in SSO that was launched on Mon, 12 Jun 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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56996 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-SAT2
1 56996U 23084BY 26253.22511521 .00002717 00000-0 30986-3 0 9995
2 56996 98.1601 35.1832 0056512 180.1455 179.9753 14.85862998166001Epoch: 2026-09-10T05:24Z
TLE epoch observation values (Epoch: 2026-09-10T05:24:09.954Z)
Latitude
0.00004°
Longitude
-35.12416°
Altitude
653.405 km
Speed
7.51 km/s
True Right ascension
02h 20m 43s
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
03:12:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
647.403 km
Perigee altitude
568.444 km
Semi-major axis
6,986.06 km
Eccentricity
0.00565
Inclination
98.1601°
RAAN
35.1832°
Arg. of periapsis
180.1455°
True anomaly
179.97558°
Mean anomaly
179.9753°
Eccentric anomaly
179.97544°
Mean motion
3.71702 °/min
Orbital period
96.85 mins
BSTAR
0.00030986
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Other satellites on launch #84 in the year 2023 (2023-06-12 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-SAT2 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 | 2026-09-10 22:08:13.120Z | 25.07° NE | 2026-09-10 22:12:13.120Z | 123.238° SE | 48.763° | 2026-09-10 22:15:13.120Z | 174.881° S |
| 6 mins | 2026-09-11 09:01:13.120Z | 131.561° SE | 2026-09-11 09:04:13.120Z | 67.67° E | 38.786° | 2026-09-11 09:07:13.120Z | 9.201° NNE |
| 4 mins | 2026-09-11 10:38:13.120Z | 235.629° WSW | 2026-09-11 10:40:13.120Z | 268.153° W | 18.431° | 2026-09-11 10:42:13.120Z | 299.755° NW |
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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