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 spacecraft
Bus & Motor
STARLIGHTB, Unknown motor
Mass
40 kg wet, ~40 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 TIANQI 38
1 67477U 26010B 26065.69187896 .00000053 00000-0 12442-3 0 9997
2 67477 44.9775 177.5658 0011310 209.1358 150.8844 13.99120872 7045Epoch: 2026-03-06T16:36Z
TLE epoch observation values (Epoch: 2026-03-06T16:36:18.342Z)
Latitude
-0.00003°
Longitude
124.0651°
Altitude
904.027 km
Speed
7.398 km/s
True Right ascension
11h 50m 15s
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
12:37:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
906.592 km
Perigee altitude
890.133 km
Semi-major axis
7,276.5 km
Eccentricity
0.00113
Inclination
44.9775°
RAAN
177.5658°
Arg. of periapsis
209.1358°
True anomaly
150.94738°
Mean anomaly
150.8844°
Eccentric anomaly
150.9159°
Mean motion
3.49671 °/min
Orbital period
102.95 mins
BSTAR
0.00012442
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-03-07 09:53:56.444Z | 208.105° SW | 2026-03-07 09:58:56.444Z | 148.212° SSE | 32.411° | 2026-03-07 10:03:56.444Z | 79.149° E |
| 10 mins | 2026-03-07 11:42:56.444Z | 256.082° W | 2026-03-07 11:46:56.444Z | 308.674° NW | 43.898° | 2026-03-07 11:52:56.444Z | 66.154° ENE |
| 10 mins | 2026-03-07 13:31:56.444Z | 289.904° WNW | 2026-03-07 13:35:56.444Z | 356.144° N | 38.683° | 2026-03-07 13:41:56.444Z | 77.27° E |
| 10 mins | 2026-03-07 15:19:56.444Z | 294.685° NW | 2026-03-07 15:24:56.444Z | 34.25° NE | 44.371° | 2026-03-07 15:29:56.444Z | 106.659° ESE |
| 9 mins | 2026-03-07 17:08:56.444Z | 275.425° WNW | 2026-03-07 17:12:56.444Z | 216.377° SW | 31.33° | 2026-03-07 17:17:56.444Z | 154.296° SSE |
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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