Showing default

QIANFAN-49, 62250

Orbit data source: Space-Track

QIANFAN-49, 62250 is a Chinese payload satellite in LEO that was launched on Thu, 05 Dec 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
62250, 2024-232P
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SECM
Mission
Operational Commercial Communications
Bus & Motor
QIANFAN, Unknown motor
Mass
267 kg wet, ~267 kg dry
Launch date (UTC)
2024-12-05 (1 year 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: 5 hours ago

TLE from 5 hours ago
0 QIANFAN-49
1 62250U 24232P   26035.16652499  .00000025  00000-0  19293-4 0  9991
2 62250  89.0009  35.8378 0015601  46.2808 313.9632 13.50984774 75050
Epoch: 2026-02-04T03:59Z
TLE epoch observation values (Epoch: 2026-02-04T03:59:47.759Z)
Latitude
-0.00003°
Longitude
-158.4482°
Altitude
1,063.534 km
Speed
7.324 km/s
True Right ascension
02h 23m 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
10:44:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.302 km
Perigee altitude
1,054.075 km
Semi-major axis
7,443.826 km
Eccentricity
0.00156
Inclination
89.0009°
RAAN
35.8378°
Arg. of periapsis
46.2808°
True anomaly
313.83435°
Mean anomaly
313.9632°
Eccentric anomaly
313.89879°
Mean motion
3.37947 °/min
Orbital period
106.53 mins
BSTAR
0.000019293
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
|