Showing default

TIANQI 18, 64060

Orbit data source: Space-Track

TIANQI 18, 64060 is a payload satellite owned by Guodian Gaokeji (CN) in LEO that was launched on Mon, 19 May 2025 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.

Loading next visibility...
Identifier
64060, 2025-105C
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Shanghai ASES
Mission
Operational Commercial Communications
Bus & Motor
STARLIGHTB, Unknown motor
Mass
40 kg wet, ~40 kg dry
Launch date (UTC)
2025-05-19 (7 months ago)
Launch vehicle
GUSHENXING 1
Launch site
Yellow Sea Launch Area, China (YSLA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.195 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 TIANQI 18
1 64060U 25105C   25348.94866783  .00000039  00000-0  11492-3 0  9994
2 64060  44.9838 121.8369 0010721 237.0940 122.8862 13.99048594 29394
Epoch: 2025-12-14T22:46Z
TLE epoch observation values (Epoch: 2025-12-14T22:46:04.900Z)
Latitude
0.00002°
Longitude
56.46224°
Altitude
901.329 km
Speed
7.401 km/s
True Right ascension
08h 07m 20s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
13:26:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
906.414 km
Perigee altitude
890.811 km
Semi-major axis
7,276.749 km
Eccentricity
0.00107
Inclination
44.9838°
RAAN
121.8369°
Arg. of periapsis
237.094°
True anomaly
122.98929°
Mean anomaly
122.8862°
Eccentric anomaly
122.93775°
Mean motion
3.49653 °/min
Orbital period
102.96 mins
BSTAR
0.00011492
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #105 in the year 2025 (2025-05-19 UTC)

Documentation

Showing up to 5 results
|