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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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Identifier
67478, 2026-010C
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Shanghai ASES
Mission
Operational spacecraft
Bus & Motor
STARLIGHTB, Unknown motor
Mass
40 kg wet, ~40 kg dry
Launch date (UTC)
2026-01-15 (4 weeks ago)
Launch vehicle
GUSHENXING 1
Launch site
Yellow Sea Launch Area, China (YSLA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 TIANQI 39
1 67478U 26010C   26039.27859865  .00000167  00000-0  15988-3 0  9999
2 67478  44.9839 296.6613 0016488  82.3005 277.9705 14.13055169  3329
Epoch: 2026-02-08T06:41Z
TLE epoch observation values (Epoch: 2026-02-08T06:41:10.923Z)
Latitude
-0°
Longitude
57.97573°
Altitude
847.3 km
Speed
7.431 km/s
True Right ascension
19h 46m 38s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
10:13:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
862.385 km
Perigee altitude
838.548 km
Semi-major axis
7,228.604 km
Eccentricity
0.00165
Inclination
44.9839°
RAAN
296.6613°
Arg. of periapsis
82.3005°
True anomaly
277.78333°
Mean anomaly
277.9705°
Eccentric anomaly
277.87692°
Mean motion
3.53152 °/min
Orbital period
101.94 mins
BSTAR
0.00015988
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Other satellites on launch #10 in the year 2026 (2026-01-15 UTC)

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