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, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 AAC-IO1
1 68498U 26067CL 26155.25556695 .00001650 00000-0 17057-3 0 9993
2 68498 97.7546 113.6282 0004158 98.6358 261.5331 14.91442830 9797Epoch: 2026-06-04T06:08Z
TLE epoch observation values (Epoch: 2026-06-04T06:08:00.984Z)
Latitude
-0.0001°
Longitude
128.92166°
Altitude
596.905 km
Speed
7.561 km/s
True Right ascension
07h 34m 30s
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
02:37:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
593.352 km
Perigee altitude
587.557 km
Semi-major axis
6,968.592 km
Eccentricity
0.00042
Inclination
97.7546°
RAAN
113.6282°
Arg. of periapsis
98.6358°
True anomaly
261.48598°
Mean anomaly
261.5331°
Eccentric anomaly
261.50954°
Mean motion
3.731 °/min
Orbital period
96.49 mins
BSTAR
0.00017057
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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 | 2026-06-06 21:03:06.735Z | 156.017° SSE | 2026-06-06 21:07:06.735Z | 42.409° NE | 41.509° | 2026-06-06 21:10:06.735Z | 355.157° N |
| 7 mins | 2026-06-07 10:22:06.735Z | 3.454° NNE | 2026-06-07 10:26:06.735Z | 271.16° WNW | 40.17° | 2026-06-07 10:29:06.735Z | 209.488° SW |
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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