Showing default

TIANQI 25, 59909

Orbit data source: Space-Track

TIANQI 25, 59909 is a payload satellite owned by Guodian Gaokeji (CN) in LEO that was launched on Wed, 29 May 2024 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
59909, 2024-102A
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)
2024-05-29 (2 years 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: 2 days ago

TLE from 2 days ago
0 TIANQI 25
1 59909U 24102A   26171.45356916  .00000000  00000-0  88071-4 0  9995
2 59909  44.9767 247.4144 0012602 253.1297 106.8154 13.99172390105361
Epoch: 2026-06-20T10:53Z
TLE epoch observation values (Epoch: 2026-06-20T10:53:08.375Z)
Latitude
0.00001°
Longitude
175.46154°
Altitude
899.321 km
Speed
7.403 km/s
True Right ascension
16h 29m 39s
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
21:24:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
907.354 km
Perigee altitude
889.015 km
Semi-major axis
7,276.321 km
Eccentricity
0.00126
Inclination
44.9767°
RAAN
247.4144°
Arg. of periapsis
253.1297°
True anomaly
106.95357°
Mean anomaly
106.8154°
Eccentric anomaly
106.88449°
Mean motion
3.49684 °/min
Orbital period
102.95 mins
BSTAR
0.000088071
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 #102 in the year 2024 (2024-05-29 UTC)

Documentation

Showing up to 5 results
|