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: 11 hours ago
TLE from 11 hours ago
0 TIANQI-6
1 46810U 20076D 26306.34797211 .00002713 00000-0 17462-3 0 9991
2 46810 34.9991 280.0123 0010785 304.0055 55.9630 15.07957028329444Epoch: 2026-11-02T08:21Z
TLE epoch observation values (Epoch: 2026-11-02T08:21:04.790Z)
Latitude
-0.00002°
Longitude
113.11603°
Altitude
537.187 km
Speed
7.598 km/s
True Right ascension
18h 40m 02s
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
14:43:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
553.14 km
Perigee altitude
538.205 km
Semi-major axis
6,923.809 km
Eccentricity
0.00108
Inclination
34.9991°
RAAN
280.0123°
Arg. of periapsis
304.0055°
True anomaly
56.06549°
Mean anomaly
55.963°
Eccentric anomaly
56.01424°
Mean motion
3.76726 °/min
Orbital period
95.56 mins
BSTAR
0.00017462
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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 | 2026-11-03 02:03:35.891Z | 203.575° SW | 2026-11-03 02:06:35.891Z | 152.74° SSE | 20.537° | 2026-11-03 02:08:35.891Z | 118.671° SE |
| 6 mins | 2026-11-03 03:44:35.891Z | 228.563° WSW | 2026-11-03 03:46:35.891Z | 177.797° S | 39.344° | 2026-11-03 03:50:35.891Z | 104.098° ESE |
| 6 mins | 2026-11-03 05:24:35.891Z | 248.315° W | 2026-11-03 05:27:35.891Z | 176.507° S | 36.802° | 2026-11-03 05:30:35.891Z | 123.928° 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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