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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Edit Public Description
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: 6 hours ago
TLE from 6 hours ago
0 AAC-HSI-SAT2
1 56995U 23084BX 25334.87364486 .00005406 00000-0 26453-3 0 9992
2 56995 97.7974 113.3073 0013588 146.7904 213.4185 15.18564379136220Epoch: 2025-11-30T20:58Z
TLE epoch observation values (Epoch: 2025-11-30T20:58:02.915Z)
Latitude
-0.00002°
Longitude
88.81391°
Altitude
521.073 km
Speed
7.598 km/s
True Right ascension
07h 33m 13s
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
00:20:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
516.519 km
Perigee altitude
497.808 km
Semi-major axis
6,885.3 km
Eccentricity
0.00136
Inclination
97.7974°
RAAN
113.3073°
Arg. of periapsis
146.7904°
True anomaly
213.33287°
Mean anomaly
213.4185°
Eccentric anomaly
213.37567°
Mean motion
3.79891 °/min
Orbital period
94.76 mins
BSTAR
0.00026453
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-01 09:45:06.962Z | 191.635° SSW | 2025-12-01 09:47:06.962Z | 235.849° WSW | 35.189° | 2025-12-01 09:51:06.962Z | 335.467° NNW |
| 4 mins | 2025-12-01 22:51:06.962Z | 330.338° NNW | 2025-12-01 22:52:06.962Z | 303.25° NW | 27.624° | 2025-12-01 22:55:06.962Z | 229.588° WSW |
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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