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: 9 hours ago
TLE from 9 hours ago
0 TECHNOSAT
1 42829U 17042E 26035.69734306 .00005064 00000-0 36984-3 0 9991
2 42829 97.4097 198.6127 0017930 180.5648 179.5561 15.03961387466787Epoch: 2026-02-04T16:44Z
TLE epoch observation values (Epoch: 2026-02-04T16:44:10.440Z)
Latitude
-0.00004°
Longitude
172.709°
Altitude
570.197 km
Speed
7.569 km/s
True Right ascension
13h 14m 27s
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
03:35:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
564.108 km
Perigee altitude
539.258 km
Semi-major axis
6,929.82 km
Eccentricity
0.00179
Inclination
97.4097°
RAAN
198.6127°
Arg. of periapsis
180.5648°
True anomaly
179.55769°
Mean anomaly
179.5561°
Eccentric anomaly
179.55689°
Mean motion
3.76236 °/min
Orbital period
95.68 mins
BSTAR
0.00036984
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-05 10:25:18.441Z | 147.996° SSE | 2026-02-05 10:29:18.441Z | 60.874° ENE | 36.392° | 2026-02-05 10:32:18.441Z | 2.422° NNE |
| 6 mins | 2026-02-05 23:39:18.441Z | 10.665° NNE | 2026-02-05 23:41:18.441Z | 1.7° NNE | 43.694° | 2026-02-05 23:45:18.441Z | 194.345° SSW |
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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