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: 5 hours ago
TLE from 5 hours ago
0 TECHNOSAT
1 42829U 17042E 25293.60482828 .00008105 00000-0 60769-3 0 9993
2 42829 97.4016 96.1311 0018449 190.3781 169.7067 15.02782792450693Epoch: 2025-10-20T14:30Z
TLE epoch observation values (Epoch: 2025-10-20T14:30:57.163Z)
Latitude
0.00002°
Longitude
-150.91183°
Altitude
573.982 km
Speed
7.567 km/s
True Right ascension
06h 24m 31s
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
14:03:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.1 km
Perigee altitude
542.517 km
Semi-major axis
6,933.446 km
Eccentricity
0.00184
Inclination
97.4016°
RAAN
96.1311°
Arg. of periapsis
190.3781°
True anomaly
169.74439°
Mean anomaly
169.7067°
Eccentric anomaly
169.72555°
Mean motion
3.75941 °/min
Orbital period
95.76 mins
BSTAR
0.00060769
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-20 23:05:01.059Z | 42.193° NE | 2025-10-20 23:08:01.059Z | 97.339° ESE | 22.725° | 2025-10-20 23:11:01.059Z | 150.141° SSE |
| 4 mins | 2025-10-21 00:41:01.059Z | 325.849° NNW | 2025-10-21 00:43:01.059Z | 284.221° WNW | 20.578° | 2025-10-21 00:45:01.059Z | 247.67° W |
| 5 mins | 2025-10-21 11:26:01.059Z | 204.56° SW | 2025-10-21 11:28:01.059Z | 265.384° W | 34.396° | 2025-10-21 11:31:01.059Z | 329.891° NNW |
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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