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: 13 hours ago
TLE from 13 hours ago
0 TIANQI-6
1 46810U 20076D 26129.84716208 .00002734 00000-0 18091-3 0 9998
2 46810 34.9994 283.7225 0010306 195.3122 164.7276 15.06935505302794Epoch: 2026-05-09T20:19Z
TLE epoch observation values (Epoch: 2026-05-09T20:19:54.803Z)
Latitude
-0.00007°
Longitude
111.08533°
Altitude
551.368 km
Speed
7.585 km/s
True Right ascension
18h 54m 53s
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
17:22:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
555.937 km
Perigee altitude
541.659 km
Semi-major axis
6,926.935 km
Eccentricity
0.00103
Inclination
34.9994°
RAAN
283.7225°
Arg. of periapsis
195.3122°
True anomaly
164.75867°
Mean anomaly
164.7276°
Eccentric anomaly
164.74314°
Mean motion
3.76471 °/min
Orbital period
95.62 mins
BSTAR
0.00018091
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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 | 2026-05-10 14:03:35.790Z | 206.822° SW | 2026-05-10 14:06:35.790Z | 154.725° SSE | 20.678° | 2026-05-10 14:09:35.790Z | 108.449° ESE |
| 6 mins | 2026-05-10 15:44:35.790Z | 232.107° WSW | 2026-05-10 15:46:35.790Z | 184.756° SSW | 32.417° | 2026-05-10 15:50:35.790Z | 105.883° ESE |
| 5 mins | 2026-05-10 17:25:35.790Z | 238.289° WSW | 2026-05-10 17:27:35.790Z | 185.247° SSW | 29.914° | 2026-05-10 17:30:35.790Z | 128.133° SE |
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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