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: 11 hours ago
TLE from 11 hours ago
0 TIANQI-6
1 46810U 20076D 26039.92013614 .00004963 00000-0 33388-3 0 9990
2 46810 34.9987 115.0973 0010202 123.3647 236.8040 15.06118187289222Epoch: 2026-02-08T22:04Z
TLE epoch observation values (Epoch: 2026-02-08T22:04:59.762Z)
Latitude
-0.00001°
Longitude
4.82589°
Altitude
550.863 km
Speed
7.587 km/s
True Right ascension
07h 40m 23s
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
11:29:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
558.371 km
Perigee altitude
544.232 km
Semi-major axis
6,929.439 km
Eccentricity
0.00102
Inclination
34.9987°
RAAN
115.0973°
Arg. of periapsis
123.3647°
True anomaly
236.70624°
Mean anomaly
236.804°
Eccentric anomaly
236.75511°
Mean motion
3.76267 °/min
Orbital period
95.68 mins
BSTAR
0.00033388
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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 | 2026-02-09 09:28:40.613Z | 224.374° SW | 2026-02-09 09:31:40.613Z | 175.313° S | 25.799° | 2026-02-09 09:34:40.613Z | 112.414° ESE |
| 5 mins | 2026-02-09 11:10:40.613Z | 235.924° WSW | 2026-02-09 11:12:40.613Z | 179.286° S | 33.452° | 2026-02-09 11:15:40.613Z | 114.752° SE |
| 5 mins | 2026-02-09 12:51:40.613Z | 232.605° WSW | 2026-02-09 12:53:40.613Z | 184.181° SSW | 24.64° | 2026-02-09 12:56:40.613Z | 137.149° 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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