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 Civil Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 AISSAT 4
1 68454U 26067AQ 26258.86521198 .00004602 00000-0 22485-3 0 9997
2 68454 97.4671 216.0491 0007098 103.4958 256.7068 15.18722439 25698Epoch: 2026-09-15T20:45Z
TLE epoch observation values (Epoch: 2026-09-15T20:45:54.315Z)
Latitude
0.00005°
Longitude
-90.25225°
Altitude
513.915 km
Speed
7.606 km/s
True Right ascension
14h 24m 11s
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
08:16:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.558 km
Perigee altitude
501.784 km
Semi-major axis
6,884.808 km
Eccentricity
0.00071
Inclination
97.4671°
RAAN
216.0491°
Arg. of periapsis
103.4958°
True anomaly
256.62766°
Mean anomaly
256.7068°
Eccentric anomaly
256.66723°
Mean motion
3.79932 °/min
Orbital period
94.75 mins
BSTAR
0.00022485
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-17 20:21:48.618Z | 101.593° ESE | 2026-09-17 20:23:48.618Z | 64.052° ENE | 17.392° | 2026-09-17 20:25:48.618Z | 29.356° NE |
| 4 mins | 2026-09-17 21:55:48.618Z | 223.479° SW | 2026-09-17 21:57:48.618Z | 278.002° WNW | 27.593° | 2026-09-17 21:59:48.618Z | 317.296° NNW |
| 4 mins | 2026-09-18 09:26:48.618Z | 60.065° ENE | 2026-09-18 09:27:48.618Z | 82.428° E | 23.978° | 2026-09-18 09:30:48.618Z | 146.516° SSE |
| 4 mins | 2026-09-18 11:00:48.618Z | 318.13° NNW | 2026-09-18 11:01:48.618Z | 297.391° NW | 19.664° | 2026-09-18 11:04:48.618Z | 243.469° WSW |
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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