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: 18 hours ago
TLE from 18 hours ago
0 TIANQI-6
1 46810U 20076D 25340.86956273 .00007482 00000-0 51211-3 0 9998
2 46810 34.9975 147.3165 0011206 278.3821 81.5617 15.05378093279564Epoch: 2025-12-06T20:52Z
TLE epoch observation values (Epoch: 2025-12-06T20:52:10.219Z)
Latitude
-0.00007°
Longitude
118.38271°
Altitude
548.13 km
Speed
7.591 km/s
True Right ascension
09h 49m 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
12:45:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.338 km
Perigee altitude
545.803 km
Semi-major axis
6,931.708 km
Eccentricity
0.00112
Inclination
34.9975°
RAAN
147.3165°
Arg. of periapsis
278.3821°
True anomaly
81.68875°
Mean anomaly
81.5617°
Eccentric anomaly
81.62522°
Mean motion
3.76082 °/min
Orbital period
95.72 mins
BSTAR
0.00051211
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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 | 2025-12-07 16:16:29.818Z | 224.907° SW | 2025-12-07 16:18:29.818Z | 180.984° SSW | 30.305° | 2025-12-07 16:22:29.818Z | 104.334° ESE |
| 5 mins | 2025-12-07 17:57:29.818Z | 239.995° WSW | 2025-12-07 17:59:29.818Z | 186.935° SSW | 32.703° | 2025-12-07 18:02:29.818Z | 122.081° SE |
| 4 mins | 2025-12-07 19:38:29.818Z | 232.004° WSW | 2025-12-07 19:40:29.818Z | 192.516° SSW | 20.204° | 2025-12-07 19:42:29.818Z | 158.77° S |
| 4 mins | 2025-12-08 14:30:29.818Z | 185.076° SSW | 2025-12-08 14:31:29.818Z | 166.054° S | 19.534° | 2025-12-08 14:34:29.818Z | 114.56° 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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