QIANFAN-39, 62240
Orbit data source: Space-Track
QIANFAN-39, 62240 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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62240 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-39
1 62240U 24232D 25288.57598656 .00000776 00000-0 32344-3 0 9992
2 62240 89.0022 43.9472 0014033 267.8214 92.1372 14.25290770 93101Epoch: 2025-10-15T13:49Z
TLE epoch observation values (Epoch: 2025-10-15T13:49:25.238Z)
Latitude
-0.00005°
Longitude
172.24396°
Altitude
810.966 km
Speed
7.448 km/s
True Right ascension
02h 55m 47s
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
14:55:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
814.538 km
Perigee altitude
794.379 km
Semi-major axis
7,182.596 km
Eccentricity
0.0014
Inclination
89.0022°
RAAN
43.9472°
Arg. of periapsis
267.8214°
True anomaly
92.29788°
Mean anomaly
92.1372°
Eccentric anomaly
92.21754°
Mean motion
3.5655 °/min
Orbital period
100.97 mins
BSTAR
0.00032344
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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-39 Visibility forecast
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-15 21:08:39.653Z | 334.468° NNW | 2025-10-15 21:12:39.653Z | 284.399° WNW | 23.484° | 2025-10-15 21:16:39.653Z | 230.416° WSW |
| 4 mins | 2025-10-16 06:50:39.653Z | 93.667° ESE | 2025-10-16 06:52:39.653Z | 69.474° E | 13.715° | 2025-10-16 06:54:39.653Z | 46.658° ENE |
| 9 mins | 2025-10-16 08:28:39.653Z | 190.251° SSW | 2025-10-16 08:32:39.653Z | 270.14° WNW | 42.734° | 2025-10-16 08:37:39.653Z | 353.043° N |
| 6 mins | 2025-10-16 19:04:39.653Z | 43.461° NE | 2025-10-16 19:07:39.653Z | 88.591° E | 21.748° | 2025-10-16 19:10:39.653Z | 127.824° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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