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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-39
1 62240U 24232D 25324.80145143 .00000652 00000-0 27023-3 0 9999
2 62240 89.0037 39.8152 0017739 145.1992 215.0365 14.25359998 98261Epoch: 2025-11-20T19:14Z
TLE epoch observation values (Epoch: 2025-11-20T19:14:05.403Z)
Latitude
-0.00004°
Longitude
51.23907°
Altitude
820.789 km
Speed
7.437 km/s
True Right ascension
02h 39m 15s
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
01:08:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
816.967 km
Perigee altitude
791.485 km
Semi-major axis
7,182.363 km
Eccentricity
0.00177
Inclination
89.0037°
RAAN
39.8152°
Arg. of periapsis
145.1992°
True anomaly
214.92001°
Mean anomaly
215.0365°
Eccentric anomaly
214.97824°
Mean motion
3.56568 °/min
Orbital period
100.96 mins
BSTAR
0.00027023
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-21 05:27:06.614Z | 170.351° S | 2025-11-21 05:32:06.614Z | 59.917° ENE | 43.731° | 2025-11-21 05:37:06.614Z | 2.843° NNE |
| 8 mins | 2025-11-21 17:44:06.614Z | 350.176° N | 2025-11-21 17:47:06.614Z | 299.853° NW | 41.517° | 2025-11-21 17:52:06.614Z | 194.832° SSW |
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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