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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 AISTECHSAT-2
1 43768U 18099L 26235.88689102 .00004828 00000-0 25435-3 0 9999
2 43768 97.4249 282.4466 0006172 73.0700 287.1209 15.16044243422535Epoch: 2026-08-23T21:17Z
TLE epoch observation values (Epoch: 2026-08-23T21:17:07.384Z)
Latitude
-0.00001°
Longitude
-9.01067°
Altitude
519.644 km
Speed
7.604 km/s
True Right ascension
18h 49m 47s
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
21:35:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
519.036 km
Perigee altitude
510.528 km
Semi-major axis
6,892.919 km
Eccentricity
0.00062
Inclination
97.4249°
RAAN
282.4466°
Arg. of periapsis
73.07°
True anomaly
287.05329°
Mean anomaly
287.1209°
Eccentric anomaly
287.0871°
Mean motion
3.79261 °/min
Orbital period
94.92 mins
BSTAR
0.00025435
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-24 15:17:17.082Z | 47.554° ENE | 2026-08-24 15:20:17.082Z | 107.343° ESE | 20.133° | 2026-08-24 15:22:17.082Z | 142.778° SSE |
| 4 mins | 2026-08-24 16:52:17.082Z | 323.47° NNW | 2026-08-24 16:54:17.082Z | 278.037° WNW | 20.358° | 2026-08-24 16:56:17.082Z | 242.767° WSW |
| 5 mins | 2026-08-25 03:31:17.082Z | 191.296° SSW | 2026-08-25 03:33:17.082Z | 252.305° W | 38.377° | 2026-08-25 03:36:17.082Z | 334.622° 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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