AISSAT 4, 68454
Orbit data source: Space-Track
AISSAT 4, 68454 is a Norwegian 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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68454 intel report (Beta)
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Identifier
Orbit
Country
NO / NORRelated business
None
Manufacturer
UTIAS-SFL
Mission
Operational spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 AISSAT 4
1 68454U 26067AQ 26174.63943836 .00004409 00000-0 22098-3 0 9991
2 68454 97.4569 132.9550 0006919 56.3049 303.8843 15.17851092 12917Epoch: 2026-06-23T15:20Z
TLE epoch observation values (Epoch: 2026-06-23T15:20:47.474Z)
Latitude
-0.00007°
Longitude
-9.05091°
Altitude
512.766 km
Speed
7.609 km/s
True Right ascension
08h 51m 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
14:52:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
514.073 km
Perigee altitude
504.542 km
Semi-major axis
6,887.444 km
Eccentricity
0.00069
Inclination
97.4569°
RAAN
132.955°
Arg. of periapsis
56.3049°
True anomaly
303.81845°
Mean anomaly
303.8843°
Eccentric anomaly
303.85138°
Mean motion
3.79713 °/min
Orbital period
94.81 mins
BSTAR
0.00022098
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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.AISSAT 4 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 | 2026-06-24 09:19:59.163Z | 52.135° ENE | 2026-06-24 09:21:59.163Z | 90.634° ESE | 19.817° | 2026-06-24 09:24:59.163Z | 145.407° SSE |
| 4 mins | 2026-06-24 10:54:59.163Z | 316.085° NNW | 2026-06-24 10:55:59.163Z | 292.332° WNW | 21.329° | 2026-06-24 10:58:59.163Z | 237.405° WSW |
| 5 mins | 2026-06-24 21:32:59.163Z | 190.363° SSW | 2026-06-24 21:34:59.163Z | 264.867° W | 39.531° | 2026-06-24 21:37:59.163Z | 336.912° NNW |
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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