TIANQI 39, 67478
Orbit data source: Space-Track
TIANQI 39, 67478 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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67478 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: 1 week ago
TLE from 1 week ago
0 TIANQI 39
1 67478U 26010C 26164.54161418 -.00000005 00000-0 79242-4 0 9994
2 67478 44.9799 94.3237 0015620 321.2511 38.7202 14.03665883 20933Epoch: 2026-06-13T12:59Z
TLE epoch observation values (Epoch: 2026-06-13T12:59:55.465Z)
Latitude
-0.00003°
Longitude
-2.51265°
Altitude
872.286 km
Speed
7.422 km/s
True Right ascension
06h 17m 17s
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
07:20:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
893.994 km
Perigee altitude
871.312 km
Semi-major axis
7,260.79 km
Eccentricity
0.00156
Inclination
44.9799°
RAAN
94.3237°
Arg. of periapsis
321.2511°
True anomaly
38.83233°
Mean anomaly
38.7202°
Eccentric anomaly
38.77625°
Mean motion
3.50806 °/min
Orbital period
102.62 mins
BSTAR
0.000079242
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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 39 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 21:10:41.069Z | 252.607° W | 2026-06-20 21:15:41.069Z | 295.165° NW | 43.926° | 2026-06-20 21:21:41.069Z | 66.141° ENE |
| 10 mins | 2026-06-20 22:59:41.069Z | 285.846° WNW | 2026-06-20 23:04:41.069Z | 6.972° NNE | 38.414° | 2026-06-20 23:09:41.069Z | 74.266° E |
| 10 mins | 2026-06-21 00:48:41.069Z | 296.038° NW | 2026-06-21 00:52:41.069Z | 357.337° N | 43.895° | 2026-06-21 00:58:41.069Z | 105.276° ESE |
| 9 mins | 2026-06-21 02:36:41.069Z | 276.846° WNW | 2026-06-21 02:40:41.069Z | 215.828° SW | 32.792° | 2026-06-21 02:45:41.069Z | 151.63° SSE |
| 10 mins | 2026-06-21 19:19:41.069Z | 210.414° SW | 2026-06-21 19:23:41.069Z | 156.074° SSE | 34.882° | 2026-06-21 19:29:41.069Z | 73.84° 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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