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 26038.97837677 .00004162 00000-0 40775-3 0 9993
2 40075 98.3895 3.3117 0003966 343.7467 16.3622 14.92871943627466Epoch: 2026-02-07T23:28Z
TLE epoch observation values (Epoch: 2026-02-07T23:28:51.752Z)
Latitude
-0.00011°
Longitude
-126.99806°
Altitude
589.358 km
Speed
7.567 km/s
True Right ascension
00h 13m 14s
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
17:36:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.794 km
Perigee altitude
583.27 km
Semi-major axis
6,964.169 km
Eccentricity
0.0004
Inclination
98.3895°
RAAN
3.3117°
Arg. of periapsis
343.7467°
True anomaly
16.37501°
Mean anomaly
16.3622°
Eccentric anomaly
16.3686°
Mean motion
3.73456 °/min
Orbital period
96.4 mins
BSTAR
0.00040775
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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 | 2026-02-08 20:33:15.571Z | 103.005° ESE | 2026-02-08 20:35:15.571Z | 68.113° E | 18.752° | 2026-02-08 20:38:15.571Z | 20.532° NNE |
| 5 mins | 2026-02-08 22:08:15.571Z | 210.961° SW | 2026-02-08 22:10:15.571Z | 253.595° W | 27.706° | 2026-02-08 22:13:15.571Z | 318.166° NNW |
| 5 mins | 2026-02-09 09:51:15.571Z | 47.656° ENE | 2026-02-09 09:53:15.571Z | 91.986° ESE | 28.232° | 2026-02-09 09:56:15.571Z | 155.356° SSE |
| 4 mins | 2026-02-09 11:27:15.571Z | 319.48° NNW | 2026-02-09 11:28:15.571Z | 301.269° NW | 18.447° | 2026-02-09 11:31:15.571Z | 250.875° W |
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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