Showing default

QIANFAN-23, 61556

Orbit data source: Space-Track

QIANFAN-23, 61556 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
61556, 2024-185E
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: 10 hours ago

TLE from 10 hours ago
0 QIANFAN-23
1 61556U 24185E   26127.23502157  .00000521  00000-0  25502-3 0  9991
2 61556  88.9834  60.9889 0006383 189.2500 170.8572 14.16467791 90342
Epoch: 2026-05-07T05:38Z
TLE epoch observation values (Epoch: 2026-05-07T05:38:25.863Z)
Latitude
0.00001°
Longitude
111.29706°
Altitude
844.919 km
Speed
7.428 km/s
True Right ascension
04h 03m 57s
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
23:33:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
838.883 km
Perigee altitude
829.676 km
Semi-major axis
7,212.417 km
Eccentricity
0.00064
Inclination
88.9834°
RAAN
60.9889°
Arg. of periapsis
189.25°
True anomaly
170.86881°
Mean anomaly
170.8572°
Eccentric anomaly
170.86301°
Mean motion
3.54341 °/min
Orbital period
101.6 mins
BSTAR
0.00025502
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
|