AAC-IO1, 68498
Orbit data source: Space-Track
AAC-IO1, 68498 is a UK payload satellite in SSO that was launched on Mon, 30 Mar 2026 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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68498 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
None
Manufacturer
AAC ClydeSpace
Mission
Operational spacecraft
Bus & Motor
CUBESAT 4U, Unknown motor
Mass
~8 kg wet, ~8 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 AAC-IO1
1 68498U 26067CL 26171.35675502 .00001725 00000-0 17770-3 0 9996
2 68498 97.7550 129.4627 0004079 67.2453 292.9196 14.91531338 12197Epoch: 2026-06-20T08:33Z
TLE epoch observation values (Epoch: 2026-06-20T08:33:43.633Z)
Latitude
-0.00007°
Longitude
92.45836°
Altitude
595.095 km
Speed
7.563 km/s
True Right ascension
08h 37m 51s
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
07:26:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.021 km
Perigee altitude
587.337 km
Semi-major axis
6,968.316 km
Eccentricity
0.00041
Inclination
97.755°
RAAN
129.4627°
Arg. of periapsis
67.2453°
True anomaly
292.87654°
Mean anomaly
292.9196°
Eccentric anomaly
292.89807°
Mean motion
3.73122 °/min
Orbital period
96.48 mins
BSTAR
0.0001777
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Other satellites on launch #67 in the year 2026 (2026-03-30 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-IO1 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 | 2026-06-21 21:42:15.294Z | 190.612° SSW | 2026-06-21 21:46:15.294Z | 265.652° W | 33.062° | 2026-06-21 21:49:15.294Z | 327.56° NNW |
| 6 mins | 2026-06-22 09:27:15.294Z | 46.813° ENE | 2026-06-22 09:29:15.294Z | 86.099° E | 25.9° | 2026-06-22 09:33:15.294Z | 158.077° S |
| 4 mins | 2026-06-22 11:03:15.294Z | 325.46° NNW | 2026-06-22 11:05:15.294Z | 287.284° WNW | 19.974° | 2026-06-22 11:07:15.294Z | 252.391° W |
| 4 mins | 2026-06-22 20:18:15.294Z | 95.922° ESE | 2026-06-22 20:20:15.294Z | 58.227° ENE | 18.405° | 2026-06-22 20:22:15.294Z | 26.506° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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