AISTECHSAT-2, 43768
Orbit data source: Space-Track
AISTECHSAT-2, 43768 is a payload satellite owned by AISTech (ES) in SSO that was launched on Mon, 03 Dec 2018 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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43768 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
AISTech
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 3 Pan, 0.3 m
Radar Cross Section
0.054 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 AISTECHSAT-2
1 43768U 18099L 25306.39939909 .00006490 00000-0 37863-3 0 9991
2 43768 97.4658 354.4185 0005370 23.3320 336.8154 15.12274239377965Epoch: 2025-11-02T09:35Z
TLE epoch observation values (Epoch: 2025-11-02T09:35:08.081Z)
Latitude
0.00003°
Longitude
168.71914°
Altitude
528.934 km
Speed
7.6 km/s
True Right ascension
23h 37m 40s
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
20:16:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
529.953 km
Perigee altitude
522.537 km
Semi-major axis
6,904.382 km
Eccentricity
0.00054
Inclination
97.4658°
RAAN
354.4185°
Arg. of periapsis
23.332°
True anomaly
336.79116°
Mean anomaly
336.8154°
Eccentric anomaly
336.80328°
Mean motion
3.78317 °/min
Orbital period
95.16 mins
BSTAR
0.00037863
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Other satellites on launch #99 in the year 2018 (2018-12-03 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.AISTECHSAT-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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-03 03:10:28.940Z | 156.18° SSE | 2025-11-03 03:14:28.940Z | 34.216° NE | 39.792° | 2025-11-03 03:17:28.940Z | 355.163° N |
| 5 mins | 2025-11-03 16:20:28.940Z | 3.022° NNE | 2025-11-03 16:22:28.940Z | 255.537° W | 43.53° | 2025-11-03 16:25:28.940Z | 200.034° SSW |
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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