AAC-HSI-SAT2, 56995
Orbit data source: Space-Track
AAC-HSI-SAT2, 56995 is a UK payload satellite 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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56995 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
AAC ClydeSpace
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.092 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-HSI-SAT2
1 56995U 23084BX 26264.28052027 .00002187 00000-0 10201-3 0 9992
2 56995 97.8381 58.2534 0011336 206.9159 153.1489 15.20981710180942Epoch: 2026-09-21T06:43Z
TLE epoch observation values (Epoch: 2026-09-21T06:43:56.951Z)
Latitude
0.00002°
Longitude
-42.89651°
Altitude
512.92 km
Speed
7.603 km/s
True Right ascension
03h 53m 00s
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
06:57:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.659 km
Perigee altitude
492.065 km
Semi-major axis
6,877.999 km
Eccentricity
0.00113
Inclination
97.8381°
RAAN
58.2534°
Arg. of periapsis
206.9159°
True anomaly
153.2075°
Mean anomaly
153.1489°
Eccentric anomaly
153.17821°
Mean motion
3.80496 °/min
Orbital period
94.61 mins
BSTAR
0.00010201
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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-HSI-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 | 2026-09-21 23:04:39.863Z | 19.316° NNE | 2026-09-21 23:08:39.863Z | 141.389° SSE | 56.425° | 2026-09-21 23:11:39.863Z | 182.956° SSW |
| 5 mins | 2026-09-22 09:43:39.863Z | 114.842° SE | 2026-09-22 09:45:39.863Z | 69.359° E | 26.25° | 2026-09-22 09:48:39.863Z | 13.715° 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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