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: 9 hours ago
TLE from 9 hours ago
0 AISTECHSAT-2
1 43768U 18099L 25323.86561220 .00006182 00000-0 35742-3 0 9991
2 43768 97.4622 11.4954 0003685 318.8268 41.2684 15.12627838380607Epoch: 2025-11-19T20:46Z
TLE epoch observation values (Epoch: 2025-11-19T20:46:28.894Z)
Latitude
-0.00005°
Longitude
0.74381°
Altitude
529.355 km
Speed
7.599 km/s
True Right ascension
00h 45m 58s
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
02:59:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
527.712 km
Perigee altitude
522.624 km
Semi-major axis
6,903.305 km
Eccentricity
0.00037
Inclination
97.4622°
RAAN
11.4954°
Arg. of periapsis
318.8268°
True anomaly
41.29626°
Mean anomaly
41.2684°
Eccentric anomaly
41.28233°
Mean motion
3.78406 °/min
Orbital period
95.14 mins
BSTAR
0.00035742
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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 | 2025-11-20 16:23:35.479Z | 2.669° NNE | 2025-11-20 16:26:35.479Z | 264.221° W | 41.533° | 2025-11-20 16:29:35.479Z | 204.658° SW |
| 6 mins | 2025-11-21 03:04:35.479Z | 146.353° SSE | 2025-11-21 03:07:35.479Z | 52.606° ENE | 37.541° | 2025-11-21 03:10:35.479Z | 359.424° N |
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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