TIANQI-6, 46810
Orbit data source: Space-Track
TIANQI-6, 46810 is a payload satellite owned by Guodian Gaokeji (CN) in LEO that was launched on Mon, 26 Oct 2020 UTC via a CHANG ZHENG 2C launch vehicle from the Xichang Space Center, China (XSC). 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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46810 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Shanghai ASES
Mission
Operational Commercial Communications
Bus & Motor
STARLIGHTB, Unknown motor
Mass
40 kg wet, ~40 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.195 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 TIANQI-6
1 46810U 20076D 25311.28682047 .00007241 00000-0 50122-3 0 9990
2 46810 35.0007 328.3178 0009886 12.4959 347.5994 15.04980632275103Epoch: 2025-11-07T06:53Z
TLE epoch observation values (Epoch: 2025-11-07T06:53:01.288Z)
Latitude
-0.00001°
Longitude
178.32946°
Altitude
543.792 km
Speed
7.596 km/s
True Right ascension
21h 53m 16s
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
08:39:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.643 km
Perigee altitude
547.936 km
Semi-major axis
6,932.927 km
Eccentricity
0.00099
Inclination
35.0007°
RAAN
328.3178°
Arg. of periapsis
12.4959°
True anomaly
347.57504°
Mean anomaly
347.5994°
Eccentric anomaly
347.58722°
Mean motion
3.75983 °/min
Orbital period
95.75 mins
BSTAR
0.00050122
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Other satellites on launch #76 in the year 2020 (2020-10-26 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.TIANQI-6 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 | 2025-11-08 05:25:48.608Z | 215.907° SW | 2025-11-08 05:28:48.608Z | 158.844° S | 24.435° | 2025-11-08 05:31:48.608Z | 107.83° ESE |
| 6 mins | 2025-11-08 07:06:48.608Z | 239.968° WSW | 2025-11-08 07:08:48.608Z | 198.706° SSW | 32.534° | 2025-11-08 07:12:48.608Z | 110.064° ESE |
| 5 mins | 2025-11-08 08:47:48.608Z | 242.606° WSW | 2025-11-08 08:49:48.608Z | 199.978° SSW | 26.936° | 2025-11-08 08:52:48.608Z | 138.817° SSE |
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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