TIANQI 37, 67476
Orbit data source: Space-Track
TIANQI 37, 67476 is a payload satellite owned by Guodian Gaokeji (CN) in LEO that was launched on Thu, 15 Jan 2026 UTC via a GUSHENXING 1 launch vehicle from the Yellow Sea Launch Area, China (YSLA). 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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67476 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, 0.6 m
Radar Cross Section
0.195 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 TIANQI 37
1 67476U 26010A 26171.03233703 .00000016 00000-0 98805-4 0 9998
2 67476 44.9829 69.0781 0012552 339.1275 20.9044 13.99164893 21795Epoch: 2026-06-20T00:46Z
TLE epoch observation values (Epoch: 2026-06-20T00:46:33.919Z)
Latitude
-0.00001°
Longitude
149.18398°
Altitude
888.158 km
Speed
7.414 km/s
True Right ascension
04h 36m 18s
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
07:20:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
907.343 km
Perigee altitude
889.076 km
Semi-major axis
7,276.346 km
Eccentricity
0.00126
Inclination
44.9829°
RAAN
69.0781°
Arg. of periapsis
339.1275°
True anomaly
20.9558°
Mean anomaly
20.9044°
Eccentric anomaly
20.93009°
Mean motion
3.49682 °/min
Orbital period
102.95 mins
BSTAR
0.000098805
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Other satellites on launch #10 in the year 2026 (2026-01-15 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 37 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-06-20 21:35:08.491Z | 256.095° W | 2026-06-20 21:40:08.491Z | 313.765° NW | 43.661° | 2026-06-20 21:46:08.491Z | 66.161° ENE |
| 10 mins | 2026-06-20 23:25:08.491Z | 290.671° WNW | 2026-06-20 23:29:08.491Z | 357.277° N | 38.677° | 2026-06-20 23:35:08.491Z | 78.057° E |
| 10 mins | 2026-06-21 01:13:08.491Z | 294.547° NW | 2026-06-21 01:18:08.491Z | 41.844° NE | 44.541° | 2026-06-21 01:23:08.491Z | 108.2° ESE |
| 9 mins | 2026-06-21 03:02:08.491Z | 274.228° WNW | 2026-06-21 03:06:08.491Z | 215.804° SW | 30.456° | 2026-06-21 03:11:08.491Z | 155.831° SSE |
| 10 mins | 2026-06-21 19:48:08.491Z | 218.119° SW | 2026-06-21 19:53:08.491Z | 136.038° SSE | 38.376° | 2026-06-21 19:58:08.491Z | 73.04° E |
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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