AISSAT 2, 40075
Orbit data source: Space-Track
AISSAT 2, 40075 is a payload satellite owned by NSC (NO) in SSO that was launched on Tue, 08 Jul 2014 UTC via a SOYUZ-2-1B launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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40075 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
UTIAS-SFL
Mission
Non-operational Civil Communications
Bus & Motor
GNB, Unknown motor
Mass
7 kg wet, 7 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Ant, 1.0 m
Radar Cross Section
0.093 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 AISSAT 2
1 40075U 14037G 25301.46807899 .00004152 00000-0 41535-3 0 9996
2 40075 98.3729 254.2605 0003616 312.6316 47.4596 14.92033807612177Epoch: 2025-10-28T11:14Z
TLE epoch observation values (Epoch: 2025-10-28T11:14:02.024Z)
Latitude
-0.00002°
Longitude
48.69693°
Altitude
592.914 km
Speed
7.564 km/s
True Right ascension
16h 57m 02s
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
08:22:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.161 km
Perigee altitude
586.122 km
Semi-major axis
6,966.778 km
Eccentricity
0.00036
Inclination
98.3729°
RAAN
254.2605°
Arg. of periapsis
312.6316°
True anomaly
47.49014°
Mean anomaly
47.4596°
Eccentric anomaly
47.47487°
Mean motion
3.73246 °/min
Orbital period
96.45 mins
BSTAR
0.00041535
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Other satellites on launch #37 in the year 2014 (2014-07-08 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 2 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-29 21:10:32.099Z | 182.086° SSW | 2025-10-29 21:12:32.099Z | 241.254° WSW | 42.279° | 2025-10-29 21:16:32.099Z | 340.453° N |
| 4 mins | 2025-10-30 08:54:32.099Z | 69.882° E | 2025-10-30 08:55:32.099Z | 86.821° E | 16.378° | 2025-10-30 08:58:32.099Z | 134.292° SE |
| 5 mins | 2025-10-30 10:29:32.099Z | 339.312° N | 2025-10-30 10:31:32.099Z | 288.45° WNW | 30.571° | 2025-10-30 10:34:32.099Z | 227.86° 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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