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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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: 20 hours ago
TLE from 20 hours ago
0 AISSAT 2
1 40075U 14037G 26205.48622050 .00002376 00000-0 23079-3 0 9995
2 40075 98.4072 181.1021 0005740 127.1156 233.0587 14.93682073652319Epoch: 2026-07-24T11:40Z
TLE epoch observation values (Epoch: 2026-07-24T11:40:09.451Z)
Latitude
-0.00001°
Longitude
63.85056°
Altitude
591.895 km
Speed
7.563 km/s
True Right ascension
12h 04m 24s
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
20:32:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.509 km
Perigee altitude
579.517 km
Semi-major axis
6,961.65 km
Eccentricity
0.00057
Inclination
98.4072°
RAAN
181.1021°
Arg. of periapsis
127.1156°
True anomaly
233.00615°
Mean anomaly
233.0587°
Eccentric anomaly
233.03242°
Mean motion
3.73659 °/min
Orbital period
96.34 mins
BSTAR
0.00023079
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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 | 2026-07-25 10:45:05.798Z | 36.502° NE | 2026-07-25 10:48:05.798Z | 89.803° E | 28.039° | 2026-07-25 10:51:05.798Z | 155.002° SSE |
| 4 mins | 2026-07-25 12:22:05.798Z | 319.79° NNW | 2026-07-25 12:23:05.798Z | 301.661° NW | 18.069° | 2026-07-25 12:26:05.798Z | 251.166° W |
| 4 mins | 2026-07-25 21:36:05.798Z | 97.833° ESE | 2026-07-25 21:37:05.798Z | 77.611° E | 21.422° | 2026-07-25 21:40:05.798Z | 21.697° NNE |
| 5 mins | 2026-07-25 23:11:05.798Z | 226.194° WSW | 2026-07-25 23:13:05.798Z | 271.479° WNW | 23.764° | 2026-07-25 23:16:05.798Z | 320.021° 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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