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: 2 days ago
TLE from 2 days ago
0 AAC-AIS-SAT2
1 56996U 23084BY 26155.29642141 .00003816 00000-0 43644-3 0 9992
2 56996 98.1475 294.8967 0057934 139.0386 221.5202 14.85420967151461Epoch: 2026-06-04T07:06Z
TLE epoch observation values (Epoch: 2026-06-04T07:06:50.809Z)
Latitude
-0.00005°
Longitude
-64.55772°
Altitude
645.717 km
Speed
7.519 km/s
True Right ascension
19h 39m 35s
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
15:20:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
649.791 km
Perigee altitude
568.829 km
Semi-major axis
6,987.447 km
Eccentricity
0.00579
Inclination
98.1475°
RAAN
294.8967°
Arg. of periapsis
139.0386°
True anomaly
221.08251°
Mean anomaly
221.5202°
Eccentric anomaly
221.30112°
Mean motion
3.71591 °/min
Orbital period
96.88 mins
BSTAR
0.00043644
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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 | 2026-06-06 09:20:51.423Z | 168.389° S | 2026-06-06 09:24:51.423Z | 294.344° NW | 44.751° | 2026-06-06 09:28:51.423Z | 345.735° N |
| 5 mins | 2026-06-06 22:44:51.423Z | 342.209° N | 2026-06-06 22:46:51.423Z | 289.294° WNW | 31.913° | 2026-06-06 22:49:51.423Z | 224.72° 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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