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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-39
1 62240U 24232D 25339.96509850 .00000808 00000-0 33600-3 0 9992
2 62240 89.0023 38.0841 0018489 100.9385 259.3889 14.25382094100427Epoch: 2025-12-05T23:09Z
TLE epoch observation values (Epoch: 2025-12-05T23:09:44.510Z)
Latitude
-0.00006°
Longitude
-24.35099°
Altitude
812.74 km
Speed
7.446 km/s
True Right ascension
02h 32m 20s
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
05:11:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
817.431 km
Perigee altitude
790.872 km
Semi-major axis
7,182.289 km
Eccentricity
0.00185
Inclination
89.0023°
RAAN
38.0841°
Arg. of periapsis
100.9385°
True anomaly
259.18074°
Mean anomaly
259.3889°
Eccentric anomaly
259.28481°
Mean motion
3.56573 °/min
Orbital period
100.96 mins
BSTAR
0.000336
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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
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-06 14:56:06.832Z | 51.706° ENE | 2025-12-06 14:58:06.832Z | 74.961° E | 13.09° | 2025-12-06 15:00:06.832Z | 98.843° ESE |
| 8 mins | 2025-12-06 16:36:06.832Z | 352.383° N | 2025-12-06 16:40:06.832Z | 251.18° W | 42.393° | 2025-12-06 16:44:06.832Z | 193.919° SSW |
| 8 mins | 2025-12-07 03:56:06.832Z | 147.188° SSE | 2025-12-07 03:59:06.832Z | 98.294° ESE | 34.924° | 2025-12-07 04:04:06.832Z | 13.675° NNE |
| 6 mins | 2025-12-07 05:38:06.832Z | 243.456° WSW | 2025-12-07 05:41:06.832Z | 284.622° WNW | 18.845° | 2025-12-07 05:44:06.832Z | 322.18° NNW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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