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 Commercial Science
Bus & Motor
CUBESAT 4U, Unknown motor
Mass
~8 kg wet, ~8 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Rod, 1.0 m
Radar Cross Section
0.045 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 AAC-IO1
1 68498U 26067CL 26258.82433747 .00001329 00000-0 13686-3 0 9999
2 68498 97.7633 215.5609 0004126 103.8718 256.2960 14.91933885 25234Epoch: 2026-09-15T19:47Z
TLE epoch observation values (Epoch: 2026-09-15T19:47:02.757Z)
Latitude
-0.00002°
Longitude
-75.98532°
Altitude
595.63 km
Speed
7.562 km/s
True Right ascension
14h 22m 14s
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
05:13:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.799 km
Perigee altitude
586.05 km
Semi-major axis
6,967.062 km
Eccentricity
0.00041
Inclination
97.7633°
RAAN
215.5609°
Arg. of periapsis
103.8718°
True anomaly
256.25007°
Mean anomaly
256.296°
Eccentric anomaly
256.27303°
Mean motion
3.73223 °/min
Orbital period
96.46 mins
BSTAR
0.00013686
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-17 20:13:36.287Z | 107.323° ESE | 2026-09-17 20:16:36.287Z | 58.254° ENE | 18.191° | 2026-09-17 20:18:36.287Z | 27.528° NE |
| 5 mins | 2026-09-17 21:49:36.287Z | 215.131° SW | 2026-09-17 21:51:36.287Z | 268.021° W | 34.947° | 2026-09-17 21:54:36.287Z | 324.729° NNW |
| 5 mins | 2026-09-18 09:32:36.287Z | 46.077° ENE | 2026-09-18 09:34:36.287Z | 91.858° ESE | 34.083° | 2026-09-18 09:37:36.287Z | 156.234° SSE |
| 4 mins | 2026-09-18 11:08:36.287Z | 319.437° NNW | 2026-09-18 11:09:36.287Z | 302.021° NW | 18.541° | 2026-09-18 11:12:36.287Z | 252.291° W |
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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