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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Edit Public Description
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: 11 hours ago
TLE from 11 hours ago
0 TECHNOSAT
1 42829U 17042E 25340.60504341 .00007493 00000-0 55395-3 0 9999
2 42829 97.4026 141.0758 0018711 33.0292 327.2098 15.03333064457755Epoch: 2025-12-06T14:31Z
TLE epoch observation values (Epoch: 2025-12-06T14:31:15.750Z)
Latitude
-0.0001°
Longitude
-152.3702°
Altitude
548.792 km
Speed
7.594 km/s
True Right ascension
09h 24m 18s
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
23:23:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
566.585 km
Perigee altitude
540.645 km
Semi-major axis
6,931.752 km
Eccentricity
0.00187
Inclination
97.4026°
RAAN
141.0758°
Arg. of periapsis
33.0292°
True anomaly
327.09345°
Mean anomaly
327.2098°
Eccentric anomaly
327.15165°
Mean motion
3.76079 °/min
Orbital period
95.72 mins
BSTAR
0.00055395
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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 | 2025-12-07 11:25:37.916Z | 208.691° SW | 2025-12-07 11:27:37.916Z | 261.11° W | 30.506° | 2025-12-07 11:30:37.916Z | 325.888° NNW |
| 5 mins | 2025-12-07 23:03:37.916Z | 52.032° ENE | 2025-12-07 23:05:37.916Z | 96.514° ESE | 24.808° | 2025-12-07 23:08:37.916Z | 152.136° SSE |
| 4 mins | 2025-12-08 00:38:37.916Z | 324.29° NNW | 2025-12-08 00:40:37.916Z | 284.558° WNW | 19.524° | 2025-12-08 00:42:37.916Z | 249.688° W |
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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