Showing default

QIANFAN-28, 61561

Orbit data source: Space-Track

QIANFAN-28, 61561 is a Chinese payload satellite in LEO that was launched on Tue, 15 Oct 2024 UTC via a CHANG ZHENG 6A launch vehicle from the Taiyaun Space Center, China (TSC). 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
61561, 2024-185K
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
GESIH/SECM
Mission
Partially operational Commercial Communications
Bus & Motor
QIANFAN, Unknown motor
Mass
267 kg wet, ~267 kg dry
Launch date (UTC)
2024-10-15 (11 months ago)
Launch vehicle
CHANG ZHENG 6A
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 5.0 m
Radar Cross Section
13.200 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 QIANFAN-28
1 61561U 24185K   25243.22378089  .00001067  00000-0  42702-3 0  9996
2 61561  88.9767  89.0900 0004907 272.8634  87.1999 14.27723939 55408
Epoch: 2025-08-31T05:22Z
TLE epoch observation values (Epoch: 2025-08-31T05:22:14.668Z)
Latitude
-0.00002°
Longitude
28.88208°
Altitude
802.243 km
Speed
7.452 km/s
True Right ascension
05h 56m 21s
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
08:47:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
799.81 km
Perigee altitude
792.769 km
Semi-major axis
7,174.426 km
Eccentricity
0.00049
Inclination
88.9767°
RAAN
89.09°
Arg. of periapsis
272.8634°
True anomaly
87.25606°
Mean anomaly
87.1999°
Eccentric anomaly
87.22798°
Mean motion
3.5716 °/min
Orbital period
100.8 mins
BSTAR
0.00042702
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...

Documentation

Showing up to 5 results
|