AAC-HSI-SAT1, 56225
Orbit data source: Space-Track
AAC-HSI-SAT1, 56225 is a UK payload satellite in SSO that was launched on Sat, 15 Apr 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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56225 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: 10 hours ago
TLE from 10 hours ago
0 AAC-HSI-SAT1
1 56225U 23054AZ 26303.89767847 .00001085 00000-0 65052-4 0 9990
2 56225 97.3457 175.4569 0010450 24.3469 335.8254 15.12940467195882Epoch: 2026-10-30T21:32Z
TLE epoch observation values (Epoch: 2026-10-30T21:32:39.419Z)
Latitude
-0.00005°
Longitude
173.0815°
Altitude
523.737 km
Speed
7.605 km/s
True Right ascension
11h 41m 49s
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
03:16:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.424 km
Perigee altitude
516.998 km
Semi-major axis
6,902.348 km
Eccentricity
0.00105
Inclination
97.3457°
RAAN
175.4569°
Arg. of periapsis
24.3469°
True anomaly
335.7763°
Mean anomaly
335.8254°
Eccentric anomaly
335.80086°
Mean motion
3.78484 °/min
Orbital period
95.12 mins
BSTAR
0.000065052
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Other satellites on launch #54 in the year 2023 (2023-04-15 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-SAT1 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 | 2026-10-31 15:08:22.628Z | 136.097° SSE | 2026-10-31 15:11:22.628Z | 68.137° E | 36.426° | 2026-10-31 15:14:22.628Z | 7.892° NNE |
| 5 mins | 2026-11-01 04:17:22.628Z | 26.571° NE | 2026-11-01 04:19:22.628Z | 117.113° SE | 64.218° | 2026-11-01 04:22:22.628Z | 181.688° SSW |
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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