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: 6 hours ago
TLE from 6 hours ago
0 AISSAT 2
1 40075U 14037G 25353.83631090 .00002420 00000-0 24202-3 0 9990
2 40075 98.3817 309.9313 0006038 117.6617 242.5214 14.92478199619985Epoch: 2025-12-19T20:04Z
TLE epoch observation values (Epoch: 2025-12-19T20:04:17.261Z)
Latitude
-0.00001°
Longitude
-79.81237°
Altitude
595.179 km
Speed
7.561 km/s
True Right ascension
20h 39m 43s
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
00:39:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.463 km
Perigee altitude
583.052 km
Semi-major axis
6,965.395 km
Eccentricity
0.0006
Inclination
98.3817°
RAAN
309.9313°
Arg. of periapsis
117.6617°
True anomaly
242.46004°
Mean anomaly
242.5214°
Eccentric anomaly
242.49072°
Mean motion
3.73357 °/min
Orbital period
96.42 mins
BSTAR
0.00024202
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-20 09:30:49.314Z | 35.896° NE | 2025-12-20 09:34:49.314Z | 110.218° ESE | 26.09° | 2025-12-20 09:37:49.314Z | 158.423° S |
| 4 mins | 2025-12-20 11:07:49.314Z | 326.796° NNW | 2025-12-20 11:09:49.314Z | 289.092° WNW | 19.59° | 2025-12-20 11:11:49.314Z | 254.041° W |
| 4 mins | 2025-12-20 20:22:49.314Z | 93.411° ESE | 2025-12-20 20:23:49.314Z | 73.353° E | 20.503° | 2025-12-20 20:26:49.314Z | 21.11° NNE |
| 6 mins | 2025-12-20 21:56:49.314Z | 211.612° SW | 2025-12-20 21:59:49.314Z | 274.566° WNW | 25.053° | 2025-12-20 22:02:49.314Z | 322.19° 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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