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 (2 years 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: 22 hours ago

TLE from 22 hours ago
0 QIANFAN-28
1 61561U 24185K   26306.86441819  .00000492  00000-0  19046-3 0  9995
2 61561  88.9919  38.8981 0005117 307.3180  52.7548 14.28539270116581
Epoch: 2026-11-02T20:44Z
TLE epoch observation values (Epoch: 2026-11-02T20:44:45.731Z)
Latitude
-0.00004°
Longitude
45.57224°
Altitude
797.462 km
Speed
7.456 km/s
True Right ascension
02h 35m 35s
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
14:25:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
797.226 km
Perigee altitude
789.887 km
Semi-major axis
7,171.694 km
Eccentricity
0.00051
Inclination
88.9919°
RAAN
38.8981°
Arg. of periapsis
307.318°
True anomaly
52.8015°
Mean anomaly
52.7548°
Eccentric anomaly
52.77815°
Mean motion
3.57364 °/min
Orbital period
100.74 mins
BSTAR
0.00019046
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
|