TSINGHUA SCIENCE, 46026 (Decayed)
Orbit data source: Space-Track
TSINGHUA SCIENCE, 46026 was a payload satellite owned by Tsinghua (CN) in LEO that was launched on Thu, 06 Aug 2020 UTC via a CHANG ZHENG 2D launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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46026 intel report (Beta)
TSINGHUA SCIENCE details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 7 months ago |
| Origin | |
| Manufacturer | Tsinghua |
| Mission | Decayed Amateur Science |
| Bus & Motor | TSSCI, Unknown motor |
| Mass | ~100 kg wet, ~100 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box, Unknown HBR |
| Radar Cross Section | 0.080 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 7 months ago
0 TSINGHUA SCIENCE
1 46026U 20054B 24163.19113482 .09146016 25032-5 36597-3 0 9991
2 46026 97.3073 261.8657 0015693 263.8822 96.0691 16.42180447215588Epoch: 2024-06-11T04:35Z
Definitive object data (Epoch: 2024-06-11T04:35:14.048Z)
| Latitude | -0.00001° |
| Longitude | -66.95873° |
| Altitude | 164.367 km |
| Speed | 7.807 km/s |
| True Right ascension | 17h 27m 27s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
| Apogee altitude | 167.065 km |
| Perigee altitude | 146.554 km |
| Semi-major axis | 6,534.946 km |
| Eccentricity | 0.0015693 |
| Inclination | 97.3073° |
| RAAN | 261.8657° |
| Arg. of periapsis | 263.8822° |
| True anomaly | 96.24788° |
| Mean anomaly | 96.0691° |
| Eccentric anomaly | 96.1585° |
| Mean motion | 4.10847 °/min |
| BSTAR | 0.00036597 |
| Orbital period | 87.62 mins |
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Other satellites on launch #54 in the year 2020 (2020-08-06 UTC)
| GAOFEN 9 04, 46025 |
| TSINGHUA SCIENCE, 46026 (Decayed) |
TSINGHUA SCIENCE Visibility forecast
Observer location: undefined°, undefined
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