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 | 10 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 10 hours ago
0 TECHNOSAT
1 42829U 17042E 24361.02718426 .00008177 00000-0 66730-3 0 9993
2 42829 97.3859 171.8240 0013835 138.8986 221.3283 14.99598196405892Epoch: 2024-12-26T00:39Z
Definitive object data (Epoch: 2024-12-26T00:39:08.72Z)
| Latitude | 0.00001° |
| Longitude | 67.02519° |
| Altitude | 578.424 km |
| Speed | 7.567 km/s |
| True Right ascension | 11h 27m 17s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -23.52631° |
| Longitude | 70.61832° |
| Altitude | 586.127 km |
| Speed | 7.561 km/s |
| Apparent Right ascension | 14h 59m 26s |
| Apparent Declination | -62° 56' 08" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 09:30:28 |
| Azimuth | 148.033° SSE |
| Elevation | -31.62° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 574.735 km |
| Perigee altitude | 555.523 km |
| Semi-major axis | 6,943.266 km |
| Eccentricity | 0.0013835 |
| Inclination | 97.3859° |
| RAAN | 171.824° |
| Arg. of periapsis | 138.8986° |
| True anomaly | 221.22374° |
| Mean anomaly | 221.3283° |
| Eccentric anomaly | 221.27601° |
| Mean motion | 3.75144 °/min |
| BSTAR | 0.0006673 |
| Orbital period | 95.96 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-12-26 12:00:20.659Z | 196.815° SSW | 2024-12-26 12:02:20.659Z | 263.28° W | 37.866° | 2024-12-26 12:05:20.659Z | 333.455° NNW |
| 4 mins | 2024-12-26 23:40:20.659Z | 62.039° ENE | 2024-12-26 23:42:20.659Z | 103.531° ESE | 20° | 2024-12-26 23:44:20.659Z | 138.476° SSE |
| 4 mins | 2024-12-27 01:15:20.659Z | 327.105° NNW | 2024-12-27 01:17:20.659Z | 281.165° WNW | 23.292° | 2024-12-27 01:19:20.659Z | 242.896° WSW |
Authenticating...
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