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 (1 year 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: 11 hours ago

TLE from 11 hours ago
0 TIANQI 18
1 64060U 25105C   26171.39393830  .00000041  00000-0  11659-3 0  9994
2 64060  44.9863   7.9521 0010473  46.1362 314.0335 13.99137751 55648
Epoch: 2026-06-20T09:27Z
TLE epoch observation values (Epoch: 2026-06-20T09:27:16.269Z)
Latitude
0.00004°
Longitude
-42.47484°
Altitude
891.489 km
Speed
7.411 km/s
True Right ascension
00h 31m 48s
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
07:19:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
905.923 km
Perigee altitude
890.682 km
Semi-major axis
7,276.44 km
Eccentricity
0.00105
Inclination
44.9863°
RAAN
7.9521°
Arg. of periapsis
46.1362°
True anomaly
313.94714°
Mean anomaly
314.0335°
Eccentric anomaly
313.99033°
Mean motion
3.49675 °/min
Orbital period
102.95 mins
BSTAR
0.00011659
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
|