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: 3 days ago
TLE from 3 days ago
0 AAC-HSI-SAT2
1 56995U 23084BX 26155.24693832 .00003905 00000-0 18306-3 0 9995
2 56995 97.8244 305.0107 0011374 225.3742 134.6566 15.20275725164375Epoch: 2026-06-04T05:55Z
TLE epoch observation values (Epoch: 2026-06-04T05:55:35.470Z)
Latitude
0.00002°
Longitude
-36.58104°
Altitude
513.595 km
Speed
7.604 km/s
True Right ascension
20h 20m 02s
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
08:56:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.818 km
Perigee altitude
494.167 km
Semi-major axis
6,880.129 km
Eccentricity
0.00114
Inclination
97.8244°
RAAN
305.0107°
Arg. of periapsis
225.3742°
True anomaly
134.74922°
Mean anomaly
134.6566°
Eccentric anomaly
134.70292°
Mean motion
3.80319 °/min
Orbital period
94.66 mins
BSTAR
0.00018306
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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 | 2026-06-06 23:15:23.523Z | 354.706° N | 2026-06-06 23:18:23.523Z | 267.819° W | 34.607° | 2026-06-06 23:21:23.523Z | 213.955° SW |
| 5 mins | 2026-06-07 09:53:23.523Z | 155.257° SSE | 2026-06-07 09:55:23.523Z | 112.222° ESE | 42.222° | 2026-06-07 09:58:23.523Z | 354.668° N |
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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