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: 13 hours ago
TLE from 13 hours ago
0 TIANQI-6
1 46810U 20076D 25300.67217510 .00005998 00000-0 41696-3 0 9993
2 46810 35.0010 33.2323 0011022 282.1775 77.7700 15.04849231273506Epoch: 2025-10-27T16:07Z
TLE epoch observation values (Epoch: 2025-10-27T16:07:55.928Z)
Latitude
0.00002°
Longitude
114.97863°
Altitude
549.275 km
Speed
7.59 km/s
True Right ascension
02h 12m 55s
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
00:42:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.835 km
Perigee altitude
547.551 km
Semi-major axis
6,933.33 km
Eccentricity
0.0011
Inclination
35.001°
RAAN
33.2323°
Arg. of periapsis
282.1775°
True anomaly
77.89347°
Mean anomaly
77.77°
Eccentric anomaly
77.83173°
Mean motion
3.7595 °/min
Orbital period
95.76 mins
BSTAR
0.00041696
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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 | 2025-10-28 09:52:16.419Z | 202.855° SW | 2025-10-28 09:55:16.419Z | 154.956° SSE | 18.665° | 2025-10-28 09:57:16.419Z | 120.97° SE |
| 6 mins | 2025-10-28 11:33:16.419Z | 230.529° WSW | 2025-10-28 11:35:16.419Z | 188.91° SSW | 31.227° | 2025-10-28 11:39:16.419Z | 105.876° ESE |
| 6 mins | 2025-10-28 13:14:16.419Z | 242.902° WSW | 2025-10-28 13:16:16.419Z | 195.706° SSW | 31.547° | 2025-10-28 13:20:16.419Z | 120.381° SE |
| 4 mins | 2025-10-28 14:55:16.419Z | 234.1° WSW | 2025-10-28 14:57:16.419Z | 198.629° SSW | 18.152° | 2025-10-28 14:59:16.419Z | 165.672° 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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