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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Edit Public Description
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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 AAC-AIS-SAT2
1 56996U 23084BY 26016.62279613 .00002648 00000-0 31351-3 0 9999
2 56996 98.1241 153.3231 0057489 229.9653 129.6509 14.84326093130881Epoch: 2026-01-16T14:56Z
TLE epoch observation values (Epoch: 2026-01-16T14:56:49.585Z)
Latitude
-0.00004°
Longitude
173.05707°
Altitude
644.521 km
Speed
7.522 km/s
True Right ascension
10h 13m 17s
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
07:15:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.937 km
Perigee altitude
572.557 km
Semi-major axis
6,990.884 km
Eccentricity
0.00575
Inclination
98.1241°
RAAN
153.3231°
Arg. of periapsis
229.9653°
True anomaly
130.1558°
Mean anomaly
129.6509°
Eccentric anomaly
129.90358°
Mean motion
3.71317 °/min
Orbital period
96.95 mins
BSTAR
0.00031351
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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 | 2026-01-17 08:52:09.211Z | 159.613° S | 2026-01-17 08:56:09.211Z | 20.9° NNE | 42.853° | 2026-01-17 09:00:09.211Z | 350.38° N |
| 6 mins | 2026-01-17 22:16:09.211Z | 354.663° N | 2026-01-17 22:19:09.211Z | 270.433° WNW | 36.987° | 2026-01-17 22:22:09.211Z | 215.241° 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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