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: 12 hours ago
TLE from 12 hours ago
0 TIANQI-6
1 46810U 20076D 25344.78243403 .00007375 00000-0 50415-3 0 9993
2 46810 34.9991 123.3689 0011058 310.4897 49.4848 15.05430698280159Epoch: 2025-12-10T18:46Z
TLE epoch observation values (Epoch: 2025-12-10T18:46:42.300Z)
Latitude
-0.00001°
Longitude
121.94481°
Altitude
544.128 km
Speed
7.595 km/s
True Right ascension
08h 13m 28s
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
04:55:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.074 km
Perigee altitude
545.744 km
Semi-major axis
6,931.546 km
Eccentricity
0.00111
Inclination
34.9991°
RAAN
123.3689°
Arg. of periapsis
310.4897°
True anomaly
49.58122°
Mean anomaly
49.4848°
Eccentric anomaly
49.533°
Mean motion
3.76095 °/min
Orbital period
95.72 mins
BSTAR
0.00050415
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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 | 2025-12-11 14:10:39.437Z | 214.416° SW | 2025-12-11 14:12:39.437Z | 163.776° S | 28.867° | 2025-12-11 14:15:39.437Z | 107.723° ESE |
| 6 mins | 2025-12-11 15:50:39.437Z | 244.887° WSW | 2025-12-11 15:53:39.437Z | 166.307° S | 32.62° | 2025-12-11 15:56:39.437Z | 115.8° SE |
| 5 mins | 2025-12-11 17:31:39.437Z | 240.965° WSW | 2025-12-11 17:33:39.437Z | 203.117° SW | 22.632° | 2025-12-11 17:36:39.437Z | 149.061° 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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