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). 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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46026 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
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
Shape & HBR
Box, Unknown HBR
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year 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
TLE epoch observation values (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
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
02:13:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
167.065 km
Perigee altitude
146.554 km
Semi-major axis
6,534.946 km
Eccentricity
0.00157
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
Orbital period
87.62 mins
BSTAR
0.00036597
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Other satellites on launch #54 in the year 2020 (2020-08-06 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.TSINGHUA SCIENCE Visibility
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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. |
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| This satellite is decayed. |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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