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, 0.5 m
Radar Cross Section
0.093 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 AISSAT 2
1 40075U 14037G 25260.82242451 .00002847 00000-0 28967-3 0 9990
2 40075 98.3646 211.1205 0006556 75.5407 284.6537 14.91632907606117Epoch: 2025-09-17T19:44Z
TLE epoch observation values (Epoch: 2025-09-17T19:44:17.477Z)
Latitude
-0.00003°
Longitude
-81.94517°
Altitude
594.713 km
Speed
7.563 km/s
True Right ascension
14h 04m 28s
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
06:32:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.459 km
Perigee altitude
585.322 km
Semi-major axis
6,968.027 km
Eccentricity
0.00066
Inclination
98.3646°
RAAN
211.1205°
Arg. of periapsis
75.5407°
True anomaly
284.581°
Mean anomaly
284.6537°
Eccentric anomaly
284.61735°
Mean motion
3.73146 °/min
Orbital period
96.48 mins
BSTAR
0.00028967
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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 | 2025-09-18 20:01:58.915Z | 120.73° SE | 2025-09-18 20:04:58.915Z | 62.522° ENE | 24.588° | 2025-09-18 20:07:58.915Z | 12.841° NNE |
| 5 mins | 2025-09-18 21:37:58.915Z | 223.024° SW | 2025-09-18 21:39:58.915Z | 259.326° W | 20.92° | 2025-09-18 21:42:58.915Z | 312.067° NW |
| 6 mins | 2025-09-19 09:20:58.915Z | 32.355° NE | 2025-09-19 09:23:58.915Z | 117.728° SE | 36.235° | 2025-09-19 09:26:58.915Z | 172.757° 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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