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). Payloads include a variety of satellites, spacecraft, and rockets 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)
TIANQI-6 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 8 hours ago |
| Origin | |
| 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 | Payload Rocket body Debris |
| Shape & HBR | Box, Unknown HBR |
| Radar Cross Section | 0.195 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 8 hours ago
0 TIANQI-6
1 46810U 20076D 24339.78602738 .00008367 00000-0 64924-3 0 9998
2 46810 34.9995 226.3914 0014149 297.3548 62.5720 15.00611935224409Epoch: 2024-12-04T18:51Z
Definitive object data (Epoch: 2024-12-04T18:51:52.765Z)
| Latitude | 0.00001° |
| Longitude | -130.65463° |
| Altitude | 559.413 km |
| Speed | 7.586 km/s |
| True Right ascension | 15h 05m 33s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 26.08955° |
| Longitude | -88.66352° |
| Altitude | 567.4 km |
| Speed | 7.58 km/s |
| Apparent Right ascension | 15h 47m 49s |
| Apparent Declination | -6° 33' 31" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 01:01:19 |
| Azimuth | 300.509° NW |
| Elevation | -40.004° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 578.055 km |
| Perigee altitude | 558.398 km |
| Semi-major axis | 6,946.364 km |
| Eccentricity | 0.0014149 |
| Inclination | 34.9995° |
| RAAN | 226.3914° |
| Arg. of periapsis | 297.3548° |
| True anomaly | 62.71603° |
| Mean anomaly | 62.572° |
| Eccentric anomaly | 62.644° |
| Mean motion | 3.74893 °/min |
| BSTAR | 0.00064924 |
| Orbital period | 96.03 mins |
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Other satellites on launch #76 in the year 2020 (2020-10-26 UTC)
| YAOGAN-30 U, 46807 |
| YAOGAN-30 V, 46808 |
| YAOGAN-30 W, 46809 |
| TIANQI-6, 46810 |
| CZ-2C R/B, 46811 |
TIANQI-6 Visibility forecast
Observer location: undefined°, undefined
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 | 2024-12-05 20:40:08.403Z | 212.821° SW | 2024-12-05 20:43:08.403Z | 155.183° SSE | 24.328° | 2024-12-05 20:46:08.403Z | 107.132° ESE |
| 6 mins | 2024-12-05 22:21:08.403Z | 240.691° WSW | 2024-12-05 22:24:08.403Z | 165.104° S | 33.686° | 2024-12-05 22:27:08.403Z | 110.666° ESE |
| 6 mins | 2024-12-06 00:02:08.403Z | 248.433° W | 2024-12-06 00:05:08.403Z | 185.072° SSW | 28.11° | 2024-12-06 00:08:08.403Z | 133.522° SE |
Authenticating...
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