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: 6 hours ago
TLE from 6 hours ago
0 TIANQI-6
1 46810U 20076D 26036.47311080 .00007165 00000-0 48152-3 0 9997
2 46810 34.9990 136.2177 0010004 90.5393 269.6463 15.06081163288708Epoch: 2026-02-05T11:21Z
TLE epoch observation values (Epoch: 2026-02-05T11:21:16.773Z)
Latitude
0.00001°
Longitude
-169.727°
Altitude
547.154 km
Speed
7.591 km/s
True Right ascension
09h 04m 52s
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
19:38:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
558.347 km
Perigee altitude
544.483 km
Semi-major axis
6,929.552 km
Eccentricity
0.001
Inclination
34.999°
RAAN
136.2177°
Arg. of periapsis
90.5393°
True anomaly
269.53167°
Mean anomaly
269.6463°
Eccentric anomaly
269.58898°
Mean motion
3.76258 °/min
Orbital period
95.68 mins
BSTAR
0.00048152
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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 | 2026-02-06 09:51:19.246Z | 191.357° SSW | 2026-02-06 09:53:19.246Z | 158.899° S | 16.593° | 2026-02-06 09:55:19.246Z | 124.978° SE |
| 6 mins | 2026-02-06 11:31:19.246Z | 229.184° WSW | 2026-02-06 11:34:19.246Z | 156.433° SSE | 29.966° | 2026-02-06 11:37:19.246Z | 106.077° ESE |
| 6 mins | 2026-02-06 13:12:19.246Z | 242.956° WSW | 2026-02-06 13:14:19.246Z | 195.552° SSW | 31.769° | 2026-02-06 13:18:19.246Z | 117.931° SE |
| 4 mins | 2026-02-06 14:53:19.246Z | 233.927° WSW | 2026-02-06 14:55:19.246Z | 195.843° SSW | 19.196° | 2026-02-06 14:57:19.246Z | 161.46° 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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