QIANFAN-42, 62243
Orbit data source: Space-Track
QIANFAN-42, 62243 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.
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62243 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Partially operational Commercial Communications
Bus & Motor
QIANFAN, Unknown motor
Mass
267 kg wet, ~267 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 5.0 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 QIANFAN-42
1 62243U 24232G 25260.22611195 .00000300 00000-0 12337-3 0 9994
2 62243 88.9972 47.2270 0015298 16.1038 344.0638 14.24350074 89058Epoch: 2025-09-17T05:25Z
TLE epoch observation values (Epoch: 2025-09-17T05:25:36.072Z)
Latitude
0.00002°
Longitude
-30.5784°
Altitude
803.162 km
Speed
7.457 km/s
True Right ascension
03h 08m 54s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
14:11:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
818.616 km
Perigee altitude
796.631 km
Semi-major axis
7,185.761 km
Eccentricity
0.00153
Inclination
88.9972°
RAAN
47.227°
Arg. of periapsis
16.1038°
True anomaly
344.01558°
Mean anomaly
344.0638°
Eccentric anomaly
344.0397°
Mean motion
3.56315 °/min
Orbital period
101.03 mins
BSTAR
0.00012337
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Other satellites on launch #232 in the year 2024 (2024-12-05 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.QIANFAN-42 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-17 22:51:46.623Z | 343.163° N | 2025-09-17 22:56:46.623Z | 266.041° W | 31.678° | 2025-09-17 23:00:46.623Z | 213.383° SW |
| 9 mins | 2025-09-18 10:12:46.623Z | 172.588° S | 2025-09-18 10:16:46.623Z | 47.133° ENE | 44.392° | 2025-09-18 10:21:46.623Z | 1.317° NNE |
| 4 mins | 2025-09-18 20:49:46.623Z | 59.459° ENE | 2025-09-18 20:50:46.623Z | 72.109° E | 15.313° | 2025-09-18 20:53:46.623Z | 108.969° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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