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: 10 hours ago
TLE from 10 hours ago
0 TIANQI-6
1 46810U 20076D 25259.46418764 .00004335 00000-0 30691-3 0 9994
2 46810 34.9998 285.1117 0011731 278.1225 81.8153 15.04243570267291Epoch: 2025-09-16T11:08Z
TLE epoch observation values (Epoch: 2025-09-16T11:08:25.812Z)
Latitude
-0°
Longitude
122.35003°
Altitude
551.597 km
Speed
7.589 km/s
True Right ascension
19h 00m 26s
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
13:24:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
565.188 km
Perigee altitude
548.916 km
Semi-major axis
6,935.189 km
Eccentricity
0.00117
Inclination
34.9998°
RAAN
285.1117°
Arg. of periapsis
278.1225°
True anomaly
81.94839°
Mean anomaly
81.8153°
Eccentric anomaly
81.88184°
Mean motion
3.75799 °/min
Orbital period
95.8 mins
BSTAR
0.00030691
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-17 04:52:39.807Z | 183.152° SSW | 2025-09-17 04:54:39.807Z | 153.166° SSE | 14.104° | 2025-09-17 04:56:39.807Z | 123.499° SE |
| 6 mins | 2025-09-17 06:32:39.807Z | 222.272° SW | 2025-09-17 06:34:39.807Z | 183.39° SSW | 28.326° | 2025-09-17 06:38:39.807Z | 105.081° ESE |
| 6 mins | 2025-09-17 08:13:39.807Z | 241.895° WSW | 2025-09-17 08:15:39.807Z | 194.886° SSW | 33.234° | 2025-09-17 08:19:39.807Z | 114.171° SE |
| 5 mins | 2025-09-17 09:54:39.807Z | 238.299° WSW | 2025-09-17 09:56:39.807Z | 198.386° SSW | 22.942° | 2025-09-17 09:59:39.807Z | 147.004° 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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