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: 8 hours ago
TLE from 8 hours ago
0 AAC-AIS-SAT2
1 56996U 23084BY 25334.83285716 .00003243 00000-0 38553-3 0 9998
2 56996 98.1216 105.6800 0059015 23.5837 336.8062 14.83907522123940Epoch: 2025-11-30T19:59Z
TLE epoch observation values (Epoch: 2025-11-30T19:59:18.858Z)
Latitude
-0.00002°
Longitude
95.91038°
Altitude
582.122 km
Speed
7.59 km/s
True Right ascension
07h 02m 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
01:22:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
655.327 km
Perigee altitude
572.798 km
Semi-major axis
6,992.2 km
Eccentricity
0.0059
Inclination
98.1216°
RAAN
105.68°
Arg. of periapsis
23.5837°
True anomaly
336.53804°
Mean anomaly
336.8062°
Eccentric anomaly
336.6723°
Mean motion
3.71212 °/min
Orbital period
96.98 mins
BSTAR
0.00038553
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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 | 2025-12-01 09:02:51.754Z | 175.286° S | 2025-12-01 09:06:51.754Z | 272.317° WNW | 42.502° | 2025-12-01 09:09:51.754Z | 339.285° N |
| 5 mins | 2025-12-01 20:51:51.754Z | 62.496° ENE | 2025-12-01 20:53:51.754Z | 98.305° ESE | 19.73° | 2025-12-01 20:56:51.754Z | 142.788° SSE |
| 6 mins | 2025-12-01 22:26:51.754Z | 345.686° N | 2025-12-01 22:29:51.754Z | 285.647° WNW | 28.756° | 2025-12-01 22:32:51.754Z | 231.429° WSW |
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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