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: 11 hours ago
TLE from 11 hours ago
0 AISSAT 2
1 40075U 14037G 26251.17061085 .00001750 00000-0 17104-3 0 9994
2 40075 98.4142 229.9788 0004712 7.8470 352.2821 14.93833920659130Epoch: 2026-09-08T04:05Z
TLE epoch observation values (Epoch: 2026-09-08T04:05:40.777Z)
Latitude
-0°
Longitude
-178.68197°
Altitude
585.766 km
Speed
7.569 km/s
True Right ascension
15h 19m 54s
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
07:42:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.321 km
Perigee altitude
579.761 km
Semi-major axis
6,961.178 km
Eccentricity
0.00047
Inclination
98.4142°
RAAN
229.9788°
Arg. of periapsis
7.847°
True anomaly
352.27484°
Mean anomaly
352.2821°
Eccentric anomaly
352.27847°
Mean motion
3.73697 °/min
Orbital period
96.33 mins
BSTAR
0.00017104
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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 | 2026-09-08 21:55:02.584Z | 123.355° SE | 2026-09-08 21:58:02.584Z | 71.573° E | 26.77° | 2026-09-08 22:01:02.584Z | 16.299° NNE |
| 4 mins | 2026-09-08 23:32:02.584Z | 234.471° WSW | 2026-09-08 23:33:02.584Z | 254.584° W | 22.704° | 2026-09-08 23:36:02.584Z | 310.264° NW |
| 6 mins | 2026-09-09 11:13:02.584Z | 32.078° NE | 2026-09-09 11:16:02.584Z | 104.416° ESE | 45.586° | 2026-09-09 11:19:02.584Z | 169.239° S |
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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