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: 15 hours ago
TLE from 15 hours ago
0 TIANQI-6
1 46810U 20076D 25292.11345846 .00009041 00000-0 62925-3 0 9997
2 46810 34.9988 85.5642 0010662 211.3897 148.6176 15.04726621272219Epoch: 2025-10-19T02:43Z
TLE epoch observation values (Epoch: 2025-10-19T02:43:22.810Z)
Latitude
-0.00005°
Longitude
16.88431°
Altitude
557.57 km
Speed
7.582 km/s
True Right ascension
05h 42m 15s
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
12:44:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.962 km
Perigee altitude
548.177 km
Semi-major axis
6,933.706 km
Eccentricity
0.00107
Inclination
34.9988°
RAAN
85.5642°
Arg. of periapsis
211.3897°
True anomaly
148.68115°
Mean anomaly
148.6176°
Eccentric anomaly
148.64938°
Mean motion
3.7592 °/min
Orbital period
95.77 mins
BSTAR
0.00062925
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-19 19:08:10.546Z | 242.211° WSW | 2025-10-19 19:10:10.546Z | 211.194° SW | 17.336° | 2025-10-19 19:13:10.546Z | 162.235° S |
| 5 mins | 2025-10-20 14:01:10.546Z | 196.345° SSW | 2025-10-20 14:03:10.546Z | 154.111° SSE | 22.465° | 2025-10-20 14:06:10.546Z | 107.411° ESE |
| 6 mins | 2025-10-20 15:41:10.546Z | 235.646° WSW | 2025-10-20 15:43:10.546Z | 190.97° SSW | 32.865° | 2025-10-20 15:47:10.546Z | 107.558° ESE |
| 5 mins | 2025-10-20 17:22:10.546Z | 241.811° WSW | 2025-10-20 17:24:10.546Z | 195.545° SSW | 29.038° | 2025-10-20 17:27:10.546Z | 133.415° 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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