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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 AISTECHSAT-2
1 43768U 18099L 26049.11977092 .00005356 00000-0 29801-3 0 9994
2 43768 97.4475 99.7680 0004725 11.9461 348.1882 15.14060860394253Epoch: 2026-02-18T02:52Z
TLE epoch observation values (Epoch: 2026-02-18T02:52:28.207Z)
Latitude
-0.00002°
Longitude
-91.43951°
Altitude
523.719 km
Speed
7.603 km/s
True Right ascension
06h 39m 04s
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
11:51:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
524.066 km
Perigee altitude
517.547 km
Semi-major axis
6,898.944 km
Eccentricity
0.00047
Inclination
97.4475°
RAAN
99.768°
Arg. of periapsis
11.9461°
True anomaly
348.17711°
Mean anomaly
348.1882°
Eccentric anomaly
348.18266°
Mean motion
3.78764 °/min
Orbital period
95.05 mins
BSTAR
0.00029801
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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 | 2026-02-18 16:07:12.771Z | 12.912° NNE | 2026-02-18 16:11:12.771Z | 183.883° SSW | 42.43° | 2026-02-18 16:14:12.771Z | 191.629° SSW |
| 5 mins | 2026-02-19 02:49:12.771Z | 122.377° SE | 2026-02-19 02:51:12.771Z | 65.37° ENE | 29.551° | 2026-02-19 02:54:12.771Z | 8.085° NNE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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