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: 11 hours ago
TLE from 11 hours ago
0 AISSAT 2
1 40075U 14037G 25255.85835225 .00001853 00000-0 19090-3 0 9997
2 40075 98.3635 205.8560 0006493 88.1157 272.0803 14.91603774605375Epoch: 2025-09-12T20:36Z
TLE epoch observation values (Epoch: 2025-09-12T20:36:01.634Z)
Latitude
-0.00006°
Longitude
-95.25083°
Altitude
595.796 km
Speed
7.562 km/s
True Right ascension
13h 43m 25s
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
23:49:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.506 km
Perigee altitude
585.457 km
Semi-major axis
6,968.118 km
Eccentricity
0.00065
Inclination
98.3635°
RAAN
205.856°
Arg. of periapsis
88.1157°
True anomaly
272.00594°
Mean anomaly
272.0803°
Eccentric anomaly
272.04312°
Mean motion
3.73138 °/min
Orbital period
96.48 mins
BSTAR
0.0001909
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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 | 2025-09-13 10:03:22.968Z | 353.635° N | 2025-09-13 10:06:22.968Z | 263.381° W | 35.756° | 2025-09-13 10:09:22.968Z | 214.917° SW |
| 6 mins | 2025-09-13 20:53:22.968Z | 176.921° S | 2025-09-13 20:55:22.968Z | 217.219° SW | 42.71° | 2025-09-13 20:59:22.968Z | 341.898° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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