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: 13 hours ago
TLE from 13 hours ago
0 AISSAT 2
1 40075U 14037G 25308.44252092 .00002981 00000-0 29965-3 0 9991
2 40075 98.3744 261.6696 0003177 283.2614 76.8249 14.92093285613215Epoch: 2025-11-04T10:37Z
TLE epoch observation values (Epoch: 2025-11-04T10:37:13.807Z)
Latitude
0.00001°
Longitude
58.43259°
Altitude
593.929 km
Speed
7.563 km/s
True Right ascension
17h 26m 40s
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
19:34:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.67 km
Perigee altitude
586.243 km
Semi-major axis
6,966.593 km
Eccentricity
0.00032
Inclination
98.3744°
RAAN
261.6696°
Arg. of periapsis
283.2614°
True anomaly
76.86035°
Mean anomaly
76.8249°
Eccentric anomaly
76.84263°
Mean motion
3.73261 °/min
Orbital period
96.45 mins
BSTAR
0.00029965
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-05 09:42:48.226Z | 20.401° NNE | 2025-11-05 09:46:48.226Z | 107.017° ESE | 41.581° | 2025-11-05 09:50:48.226Z | 183.226° SSW |
| 6 mins | 2025-11-05 20:33:48.226Z | 133.683° SE | 2025-11-05 20:36:48.226Z | 52.924° ENE | 33.087° | 2025-11-05 20:39:48.226Z | 3.348° NNE |
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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