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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AISTECHSAT-2 radio frequencies
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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: 1 day ago
TLE from 1 day ago
0 AISTECHSAT-2
1 43768U 18099L 25259.87074574 .00005766 00000-0 34487-3 0 9993
2 43768 97.4737 308.9342 0006069 149.5282 210.6302 15.11417552370936Epoch: 2025-09-16T20:53Z
TLE epoch observation values (Epoch: 2025-09-16T20:53:52.431Z)
Latitude
-0.00005°
Longitude
-0.58909°
Altitude
538.563 km
Speed
7.591 km/s
True Right ascension
20h 35m 44s
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
19:55:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
533.048 km
Perigee altitude
524.664 km
Semi-major axis
6,906.993 km
Eccentricity
0.00061
Inclination
97.4737°
RAAN
308.9342°
Arg. of periapsis
149.5282°
True anomaly
210.59479°
Mean anomaly
210.6302°
Eccentric anomaly
210.61249°
Mean motion
3.78103 °/min
Orbital period
95.21 mins
BSTAR
0.00034487
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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 | 2025-09-18 03:12:29.390Z | 156.722° SSE | 2025-09-18 03:16:29.390Z | 34.104° NE | 40.304° | 2025-09-18 03:19:29.390Z | 354.863° N |
| 6 mins | 2025-09-18 16:22:29.390Z | 4.015° NNE | 2025-09-18 16:24:29.390Z | 319.485° NNW | 42.775° | 2025-09-18 16:28:29.390Z | 200.059° 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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