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: 1 day ago
TLE from 1 day ago
0 AAC-AIS-SAT2
1 56996U 23084BY 26308.91219897 .00001469 00000-0 16985-3 0 9999
2 56996 98.1680 92.3270 0056108 1.5104 358.6269 14.86096669174278Epoch: 2026-11-04T21:53Z
TLE epoch observation values (Epoch: 2026-11-04T21:53:33.991Z)
Latitude
-0.00006°
Longitude
79.78167°
Altitude
573.961 km
Speed
7.595 km/s
True Right ascension
06h 09m 18s
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
23:12:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
646.384 km
Perigee altitude
567.997 km
Semi-major axis
6,985.328 km
Eccentricity
0.00561
Inclination
98.168°
RAAN
92.327°
Arg. of periapsis
1.5104°
True anomaly
358.61138°
Mean anomaly
358.6269°
Eccentric anomaly
358.61915°
Mean motion
3.7176 °/min
Orbital period
96.84 mins
BSTAR
0.00016985
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-11-06 09:33:31.876Z | 158.485° S | 2026-11-06 09:37:31.876Z | 61.708° ENE | 71.015° | 2026-11-06 09:41:31.876Z | 351.637° N |
| 7 mins | 2026-11-06 22:56:31.876Z | 358.763° N | 2026-11-06 22:59:31.876Z | 284.826° WNW | 56.024° | 2026-11-06 23:03:31.876Z | 209.904° SW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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