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: 14 hours ago
TLE from 14 hours ago
0 TECHNOSAT
1 42829U 17042E 25310.51627463 .00006208 00000-0 46371-3 0 9994
2 42829 97.4049 112.2997 0020107 130.4300 229.8684 15.02988048453233Epoch: 2025-11-06T12:23Z
TLE epoch observation values (Epoch: 2025-11-06T12:23:26.128Z)
Latitude
0.00003°
Longitude
-119.53264°
Altitude
569.763 km
Speed
7.571 km/s
True Right ascension
07h 29m 11s
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
22:27:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.617 km
Perigee altitude
540.737 km
Semi-major axis
6,932.814 km
Eccentricity
0.00201
Inclination
97.4049°
RAAN
112.2997°
Arg. of periapsis
130.43°
True anomaly
229.69252°
Mean anomaly
229.8684°
Eccentric anomaly
229.78043°
Mean motion
3.75992 °/min
Orbital period
95.75 mins
BSTAR
0.00046371
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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 | 2025-11-07 10:52:50.125Z | 162.79° S | 2025-11-07 10:56:50.125Z | 12.088° NNE | 42.622° | 2025-11-07 10:59:50.125Z | 350.931° N |
| 6 mins | 2025-11-08 00:06:50.125Z | 355.44° N | 2025-11-08 00:09:50.125Z | 261.61° W | 36.77° | 2025-11-08 00:12:50.125Z | 211.067° SW |
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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