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: 7 hours ago
TLE from 7 hours ago
0 AAC-AIS-SAT2
1 56996U 23084BY 26207.29471152 .00002380 00000-0 27388-3 0 9994
2 56996 98.1526 348.1178 0055858 331.9462 27.8745 14.85673196159186Epoch: 2026-07-26T07:04Z
TLE epoch observation values (Epoch: 2026-07-26T07:04:23.075Z)
Latitude
0.00003°
Longitude
-61.97305°
Altitude
580.023 km
Speed
7.589 km/s
True Right ascension
23h 12m 28s
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
03:05:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
647.544 km
Perigee altitude
569.492 km
Semi-major axis
6,986.655 km
Eccentricity
0.00559
Inclination
98.1526°
RAAN
348.1178°
Arg. of periapsis
331.9462°
True anomaly
28.17562°
Mean anomaly
27.8745°
Eccentric anomaly
28.02487°
Mean motion
3.71654 °/min
Orbital period
96.86 mins
BSTAR
0.00027388
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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 | 2026-07-26 22:11:29.323Z | 19.253° NNE | 2026-07-26 22:14:29.323Z | 56.659° ENE | 41.932° | 2026-07-26 22:18:29.323Z | 184.788° SSW |
| 6 mins | 2026-07-27 09:04:29.323Z | 140.48° SSE | 2026-07-27 09:07:29.323Z | 59.006° ENE | 36.527° | 2026-07-27 09:10:29.323Z | 1.979° NNE |
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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