TIANQI 38, 67477
Orbit data source: Space-Track
TIANQI 38, 67477 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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67477 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, 0.5 m
Radar Cross Section
0.195 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 TIANQI 38
1 67477U 26010B 26171.44327529 .00000027 00000-0 10695-3 0 9996
2 67477 44.9790 67.0216 0011151 347.4547 12.6007 13.99160572 21856Epoch: 2026-06-20T10:38Z
TLE epoch observation values (Epoch: 2026-06-20T10:38:18.985Z)
Latitude
0.00002°
Longitude
-1.21531°
Altitude
888.785 km
Speed
7.413 km/s
True Right ascension
04h 28m 05s
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
07:18:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
906.339 km
Perigee altitude
890.111 km
Semi-major axis
7,276.362 km
Eccentricity
0.00112
Inclination
44.979°
RAAN
67.0216°
Arg. of periapsis
347.4547°
True anomaly
12.62861°
Mean anomaly
12.6007°
Eccentric anomaly
12.61465°
Mean motion
3.49681 °/min
Orbital period
102.95 mins
BSTAR
0.00010695
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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 38 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 21:08:02.207Z | 246.053° WSW | 2026-06-20 21:14:02.207Z | 33.36° NE | 44.951° | 2026-06-20 21:19:02.207Z | 66.498° ENE |
| 10 mins | 2026-06-20 22:58:02.207Z | 283.25° WNW | 2026-06-20 23:03:02.207Z | 11.74° NNE | 38.53° | 2026-06-20 23:08:02.207Z | 72.12° E |
| 10 mins | 2026-06-21 00:47:02.207Z | 296.212° NW | 2026-06-21 00:51:02.207Z | 348.95° N | 42.459° | 2026-06-21 00:57:02.207Z | 99.494° ESE |
| 10 mins | 2026-06-21 02:35:02.207Z | 283.406° WNW | 2026-06-21 02:40:02.207Z | 203.858° SW | 36.543° | 2026-06-21 02:45:02.207Z | 143.634° SSE |
| 10 mins | 2026-06-21 19:22:02.207Z | 204.895° SW | 2026-06-21 19:26:02.207Z | 154.331° SSE | 32.023° | 2026-06-21 19:32:02.207Z | 75.835° 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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