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: 16 hours ago
TLE from 16 hours ago
0 AISSAT 2
1 40075U 14037G 25338.68400766 .00006498 00000-0 64094-3 0 9992
2 40075 98.3790 293.8146 0004927 159.8484 200.2928 14.92363744617727Epoch: 2025-12-04T16:24Z
TLE epoch observation values (Epoch: 2025-12-04T16:24:58.261Z)
Latitude
-0.0001°
Longitude
-26.16506°
Altitude
596.812 km
Speed
7.56 km/s
True Right ascension
19h 35m 15s
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
05:55:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.046 km
Perigee altitude
584.182 km
Semi-major axis
6,965.751 km
Eccentricity
0.00049
Inclination
98.379°
RAAN
293.8146°
Arg. of periapsis
159.8484°
True anomaly
200.27323°
Mean anomaly
200.2928°
Eccentric anomaly
200.28301°
Mean motion
3.73329 °/min
Orbital period
96.43 mins
BSTAR
0.00064094
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-05 09:05:55.023Z | 55.236° ENE | 2025-12-05 09:07:55.023Z | 86.022° E | 16.621° | 2025-12-05 09:10:55.023Z | 134.624° SE |
| 5 mins | 2025-12-05 10:41:55.023Z | 338.702° N | 2025-12-05 10:43:55.023Z | 289.014° WNW | 29.702° | 2025-12-05 10:46:55.023Z | 228.966° WSW |
| 6 mins | 2025-12-05 21:30:55.023Z | 191.028° SSW | 2025-12-05 21:33:55.023Z | 283.512° WNW | 36.59° | 2025-12-05 21:36:55.023Z | 333.64° 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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