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, Unknown HBR
Radar Cross Section
0.195 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 TIANQI-6
1 46810U 20076D 25260.19426792 .00003868 00000-0 27406-3 0 9996
2 46810 34.9996 280.6512 0011710 284.0499 75.8908 15.04248753267406Epoch: 2025-09-17T04:39Z
TLE epoch observation values (Epoch: 2025-09-17T04:39:44.748Z)
Latitude
-0.00001°
Longitude
-145.65898°
Altitude
550.759 km
Speed
7.59 km/s
True Right ascension
18h 42m 36s
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
20:48:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
565.157 km
Perigee altitude
548.915 km
Semi-major axis
6,935.173 km
Eccentricity
0.00117
Inclination
34.9996°
RAAN
280.6512°
Arg. of periapsis
284.0499°
True anomaly
76.02099°
Mean anomaly
75.8908°
Eccentric anomaly
75.95589°
Mean motion
3.758 °/min
Orbital period
95.8 mins
BSTAR
0.00027406
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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 | 2025-09-18 04:46:34.186Z | 199.148° SSW | 2025-09-18 04:49:34.186Z | 151.78° SSE | 17.489° | 2025-09-18 04:51:34.186Z | 119.815° SE |
| 6 mins | 2025-09-18 06:27:34.186Z | 227.36° WSW | 2025-09-18 06:29:34.186Z | 183.717° SSW | 30.972° | 2025-09-18 06:33:34.186Z | 104.877° ESE |
| 6 mins | 2025-09-18 08:08:34.186Z | 241.874° WSW | 2025-09-18 08:10:34.186Z | 192.526° SSW | 32.25° | 2025-09-18 08:14:34.186Z | 118.331° SE |
| 4 mins | 2025-09-18 09:49:34.186Z | 234.421° WSW | 2025-09-18 09:51:34.186Z | 197.522° SSW | 19.371° | 2025-09-18 09:53:34.186Z | 163.384° S |
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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