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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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: 5 hours ago
TLE from 5 hours ago
0 TIANQI-6
1 46810U 20076D 26126.53454301 .00004037 00000-0 26625-3 0 9994
2 46810 34.9998 304.0446 0009901 166.3517 193.7462 15.06916685302297Epoch: 2026-05-06T12:49Z
TLE epoch observation values (Epoch: 2026-05-06T12:49:44.516Z)
Latitude
0.00002°
Longitude
-112.78451°
Altitude
551.201 km
Speed
7.585 km/s
True Right ascension
20h 16m 10s
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
01:29:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
555.714 km
Perigee altitude
541.997 km
Semi-major axis
6,926.993 km
Eccentricity
0.00099
Inclination
34.9998°
RAAN
304.0446°
Arg. of periapsis
166.3517°
True anomaly
193.71927°
Mean anomaly
193.7462°
Eccentric anomaly
193.73273°
Mean motion
3.76466 °/min
Orbital period
95.63 mins
BSTAR
0.00026625
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-06 17:55:47.264Z | 245.346° WSW | 2026-05-06 17:58:47.264Z | 190.976° SSW | 32.939° | 2026-05-06 18:02:47.264Z | 108.439° ESE |
| 5 mins | 2026-05-06 19:37:47.264Z | 238.521° WSW | 2026-05-06 19:39:47.264Z | 190.055° SSW | 27.408° | 2026-05-06 19:42:47.264Z | 134.421° SE |
| 5 mins | 2026-05-07 16:08:47.264Z | 208.835° SW | 2026-05-07 16:10:47.264Z | 161.2° S | 26.59° | 2026-05-07 16:13:47.264Z | 107.629° ESE |
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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