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QIANFAN-14, 60392

Orbit data source: Space-Track

QIANFAN-14, 60392 is a Chinese payload satellite in LEO that was launched on Tue, 06 Aug 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.

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Identifier
60392, 2024-140P
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)
2024-08-06 (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: 11 hours ago

TLE from 11 hours ago
0 QIANFAN-14
1 60392U 24140P   26118.46324110  .00000054  00000-0  65233-4 0  9992
2 60392  88.9659 285.0954 0017205 167.1864 192.9728 13.51006399 85736
Epoch: 2026-04-28T11:07Z
TLE epoch observation values (Epoch: 2026-04-28T11:07:04.031Z)
Latitude
0.00002°
Longitude
-98.10959°
Altitude
1,084 km
Speed
7.304 km/s
True Right ascension
19h 00m 22s
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
05:07:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.416 km
Perigee altitude
1,052.802 km
Semi-major axis
7,443.746 km
Eccentricity
0.00172
Inclination
88.9659°
RAAN
285.0954°
Arg. of periapsis
167.1864°
True anomaly
192.92863°
Mean anomaly
192.9728°
Eccentric anomaly
192.95071°
Mean motion
3.37953 °/min
Orbital period
106.52 mins
BSTAR
0.000065233
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Computing Atmospheric mass density...

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