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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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: 14 hours ago
TLE from 14 hours ago
0 TIANQI-6
1 46810U 20076D 26197.74608679 .00001425 00000-0 94289-4 0 9994
2 46810 34.9977 227.0268 0009567 69.4841 290.6895 15.07357024313040Epoch: 2026-07-16T17:54Z
TLE epoch observation values (Epoch: 2026-07-16T17:54:21.898Z)
Latitude
-0.00001°
Longitude
23.85242°
Altitude
540.861 km
Speed
7.595 km/s
True Right ascension
15h 08m 06s
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
20:59:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
554.134 km
Perigee altitude
540.882 km
Semi-major axis
6,925.645 km
Eccentricity
0.00096
Inclination
34.9977°
RAAN
227.0268°
Arg. of periapsis
69.4841°
True anomaly
290.5869°
Mean anomaly
290.6895°
Eccentric anomaly
290.6382°
Mean motion
3.76576 °/min
Orbital period
95.6 mins
BSTAR
0.000094289
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-07-17 08:34:22.483Z | 251.564° W | 2026-07-17 08:37:22.483Z | 201.196° SSW | 32.033° | 2026-07-17 08:41:22.483Z | 115.328° SE |
| 5 mins | 2026-07-17 10:16:22.483Z | 237.058° WSW | 2026-07-17 10:18:22.483Z | 196.545° SSW | 21.844° | 2026-07-17 10:21:22.483Z | 146.709° SSE |
| 6 mins | 2026-07-18 06:46:22.483Z | 229.406° WSW | 2026-07-18 06:49:22.483Z | 154.8° SSE | 29.909° | 2026-07-18 06:52:22.483Z | 105.837° ESE |
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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