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: 7 hours ago
TLE from 7 hours ago
0 AISTECHSAT-2
1 43768U 18099L 25354.09209728 .00004575 00000-0 26190-3 0 9993
2 43768 97.4575 41.0524 0004637 182.7066 177.4141 15.13114845385175Epoch: 2025-12-20T02:12Z
TLE epoch observation values (Epoch: 2025-12-20T02:12:37.204Z)
Latitude
-0.00005°
Longitude
-81.02648°
Altitude
532.986 km
Speed
7.594 km/s
True Right ascension
02h 44m 12s
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
07:46:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.885 km
Perigee altitude
520.485 km
Semi-major axis
6,901.822 km
Eccentricity
0.00046
Inclination
97.4575°
RAAN
41.0524°
Arg. of periapsis
182.7066°
True anomaly
177.4165°
Mean anomaly
177.4141°
Eccentric anomaly
177.4153°
Mean motion
3.78528 °/min
Orbital period
95.11 mins
BSTAR
0.0002619
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-20 15:28:35.200Z | 39.113° NE | 2025-12-20 15:31:35.200Z | 92.395° ESE | 23.042° | 2025-12-20 15:34:35.200Z | 150.257° SSE |
| 4 mins | 2025-12-20 17:04:35.200Z | 317.551° NNW | 2025-12-20 17:05:35.200Z | 296.78° NW | 19.038° | 2025-12-20 17:08:35.200Z | 243.36° WSW |
| 5 mins | 2025-12-21 03:44:35.200Z | 198.941° SSW | 2025-12-21 03:46:35.200Z | 255.559° W | 34.866° | 2025-12-21 03:49:35.200Z | 330.228° NNW |
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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