Showing default

TIANQI 32, 61198

Orbit data source: Space-Track

TIANQI 32, 61198 is a payload satellite owned by Guodian Gaokeji (CN) in LEO that was launched on Fri, 20 Sep 2024 UTC via a KUAIZHOU-1A launch vehicle from the Xichang Space Center, China (XSC). 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
61198, 2024-170D
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)
2024-09-20 (1 year ago)
Launch vehicle
KUAIZHOU-1A
Launch site
Xichang Space Center, China (XSC)
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: 14 hours ago

TLE from 14 hours ago
0 TIANQI 32
1 61198U 24170D   26056.78045037  .00000051  00000-0  12276-3 0  9999
2 61198  44.8599 274.1813 0007932 270.9717  89.0205 13.99119114 68935
Epoch: 2026-02-25T18:43Z
TLE epoch observation values (Epoch: 2026-02-25T18:43:50.911Z)
Latitude
-0.00003°
Longitude
-162.42158°
Altitude
896.737 km
Speed
7.405 km/s
True Right ascension
18h 16m 43s
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
12:03:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
904.159 km
Perigee altitude
892.616 km
Semi-major axis
7,276.524 km
Eccentricity
0.00079
Inclination
44.8599°
RAAN
274.1813°
Arg. of periapsis
270.9717°
True anomaly
89.11138°
Mean anomaly
89.0205°
Eccentric anomaly
89.06594°
Mean motion
3.49669 °/min
Orbital period
102.95 mins
BSTAR
0.00012276
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 #170 in the year 2024 (2024-09-20 UTC)

Documentation

Showing up to 5 results
|