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). Payloads include a variety of satellites, spacecraft, and rockets 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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TECHNOSAT radio frequencies
TECHNOSAT details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 7 hours ago |
| Origin | |
| 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 | Payload Rocket body Debris |
| Shape & HBR | Oct Cyl, 0.45 m |
| Radar Cross Section | 0.175 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 7 hours ago
0 TECHNOSAT
1 42829U 17042E 24340.07297117 .00007870 00000-0 64768-3 0 9992
2 42829 97.3857 151.9463 0011861 217.2439 142.7963 14.99304620402758Epoch: 2024-12-05T01:45Z
Definitive object data (Epoch: 2024-12-05T01:45:04.709Z)
| Latitude | -0.00004° |
| Longitude | 51.31767° |
| Altitude | 578.674 km |
| Speed | 7.568 km/s |
| True Right ascension | 10h 07m 47s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -10.42526° |
| Longitude | -129.75489° |
| Altitude | 566.614 km |
| Speed | 7.581 km/s |
| Apparent Right ascension | 20h 47m 04s |
| Apparent Declination | -26° 11' 46" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 06:58:28 |
| Azimuth | 292.989° NW |
| Elevation | -63.588° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 574.273 km |
| Perigee altitude | 557.8 km |
| Semi-major axis | 6,944.173 km |
| Eccentricity | 0.0011861 |
| Inclination | 97.3857° |
| RAAN | 151.9463° |
| Arg. of periapsis | 217.2439° |
| True anomaly | 142.87839° |
| Mean anomaly | 142.7963° |
| Eccentric anomaly | 142.83735° |
| Mean motion | 3.7507 °/min |
| BSTAR | 0.00064768 |
| Orbital period | 95.98 mins |
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Other satellites on launch #42 in the year 2017 (2017-07-14 UTC)
TECHNOSAT Visibility forecast
Observer location: undefined°, undefined
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 | 2024-12-05 11:29:18.704Z | 153.724° SSE | 2024-12-05 11:32:18.704Z | 100.375° ESE | 40.746° | 2024-12-05 11:36:18.704Z | 356.008° N |
| 6 mins | 2024-12-06 00:45:18.704Z | 359.948° N | 2024-12-06 00:47:18.704Z | 317.522° NNW | 40.687° | 2024-12-06 00:51:18.704Z | 204.343° SW |
Authenticating...
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