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: 2 days ago
TLE from 2 days ago
0 AISSAT 2
1 40075U 14037G 25321.45171637 .00004111 00000-0 40933-3 0 9997
2 40075 98.3764 275.4940 0003510 221.1834 138.9119 14.92234296615158Epoch: 2025-11-17T10:50Z
TLE epoch observation values (Epoch: 2025-11-17T10:50:28.294Z)
Latitude
0.00001°
Longitude
56.12415°
Altitude
595.838 km
Speed
7.561 km/s
True Right ascension
18h 21m 58s
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
00:19:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.462 km
Perigee altitude
585.572 km
Semi-major axis
6,966.154 km
Eccentricity
0.00035
Inclination
98.3764°
RAAN
275.494°
Arg. of periapsis
221.1834°
True anomaly
138.93833°
Mean anomaly
138.9119°
Eccentric anomaly
138.92511°
Mean motion
3.73296 °/min
Orbital period
96.44 mins
BSTAR
0.00040933
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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 | 2025-11-19 10:03:56.061Z | 11.123° NNE | 2025-11-19 10:07:56.061Z | 308.6° NW | 44.644° | 2025-11-19 10:11:56.061Z | 197.625° SSW |
| 6 mins | 2025-11-19 20:54:56.061Z | 152.798° SSE | 2025-11-19 20:57:56.061Z | 34.921° NE | 41.484° | 2025-11-19 21:00:56.061Z | 353.611° N |
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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