Showing default

TIANQI 34, 62366

Orbit data source: Space-Track

TIANQI 34, 62366 is a payload satellite owned by Guodian Gaokeji (CN) in LEO that was launched on Thu, 19 Dec 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
62366, 2024-245B
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)
2024-12-19 (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: 10 hours ago

TLE from 10 hours ago
0 TIANQI 34
1 62366U 24245B   26171.43344513  .00000043  00000-0  11746-3 0  9993
2 62366  44.9813 307.2810 0003663  43.3944 316.7176 13.99220245 76786
Epoch: 2026-06-20T10:24Z
TLE epoch observation values (Epoch: 2026-06-20T10:24:09.659Z)
Latitude
-0.00005°
Longitude
-117.40743°
Altitude
894.554 km
Speed
7.407 km/s
True Right ascension
20h 29m 07s
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
07:12:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
900.683 km
Perigee altitude
895.352 km
Semi-major axis
7,276.155 km
Eccentricity
0.00037
Inclination
44.9813°
RAAN
307.281°
Arg. of periapsis
43.3944°
True anomaly
316.68881°
Mean anomaly
316.7176°
Eccentric anomaly
316.70321°
Mean motion
3.49696 °/min
Orbital period
102.95 mins
BSTAR
0.00011746
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 #245 in the year 2024 (2024-12-19 UTC)

Documentation

Showing up to 5 results
|