TECHNOSAT, 42829
Orbit data source: Space-Track
TECHNOSAT, 42829 is a payload satellite owned by TUB (DE) in SSO that was launched on Fri, 14 Jul 2017 UTC via a SOYUZ-2-1A launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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42829 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
TUB
Mission
Operational Amateur Technology
Bus & Motor
TUBIX20, Unknown motor
Mass
18 kg wet, 18 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Oct Cyl, 1.0 m
Radar Cross Section
0.175 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 TECHNOSAT
1 42829U 17042E 26171.44071003 .00002691 00000-0 19322-3 0 9993
2 42829 97.4297 328.9745 0019198 84.0647 276.2768 15.04979783487190Epoch: 2026-06-20T10:34Z
TLE epoch observation values (Epoch: 2026-06-20T10:34:37.346Z)
Latitude
0.00003°
Longitude
-98.33641°
Altitude
553.207 km
Speed
7.586 km/s
True Right ascension
21h 55m 53s
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
21:38:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.852 km
Perigee altitude
535.257 km
Semi-major axis
6,926.692 km
Eccentricity
0.00192
Inclination
97.4297°
RAAN
328.9745°
Arg. of periapsis
84.0647°
True anomaly
276.05807°
Mean anomaly
276.2768°
Eccentric anomaly
276.16744°
Mean motion
3.76491 °/min
Orbital period
95.62 mins
BSTAR
0.00019322
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Other satellites on launch #42 in the year 2017 (2017-07-14 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.TECHNOSAT 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 | 2026-06-22 10:36:02.356Z | 169.22° S | 2026-06-22 10:38:02.356Z | 342.008° N | 42.669° | 2026-06-22 10:41:02.356Z | 347.434° N |
| 6 mins | 2026-06-22 23:47:02.356Z | 351.614° N | 2026-06-22 23:50:02.356Z | 262.538° W | 34.036° | 2026-06-22 23:53:02.356Z | 214.42° SW |
| 5 mins | 2026-06-23 10:31:02.356Z | 163.719° S | 2026-06-23 10:34:02.356Z | 10.006° NNE | 43.768° | 2026-06-23 10:36:02.356Z | 350.759° N |
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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