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 25310.90119101 .00000797 00000-0 33206-3 0 9990
2 62240 89.0038 41.4003 0016145 188.3736 171.7190 14.25329390 96288Epoch: 2025-11-06T21:37Z
TLE epoch observation values (Epoch: 2025-11-06T21:37:42.903Z)
Latitude
-0.00003°
Longitude
30.61867°
Altitude
821.929 km
Speed
7.436 km/s
True Right ascension
02h 45m 36s
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
01:29:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
815.925 km
Perigee altitude
792.733 km
Semi-major axis
7,182.466 km
Eccentricity
0.00161
Inclination
89.0038°
RAAN
41.4003°
Arg. of periapsis
188.3736°
True anomaly
171.74559°
Mean anomaly
171.719°
Eccentric anomaly
171.7323°
Mean motion
3.5656 °/min
Orbital period
100.96 mins
BSTAR
0.00033206
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-07 06:09:58.318Z | 155.208° SSE | 2025-11-07 06:14:58.318Z | 66.45° ENE | 36.65° | 2025-11-07 06:18:58.318Z | 12.614° NNE |
| 5 mins | 2025-11-07 07:53:58.318Z | 255.167° W | 2025-11-07 07:55:58.318Z | 282.955° WNW | 18.106° | 2025-11-07 07:58:58.318Z | 320.041° NNW |
| 9 mins | 2025-11-07 18:25:58.318Z | 2.877° NNE | 2025-11-07 18:29:58.318Z | 40.35° NE | 44.646° | 2025-11-07 18:34:58.318Z | 179.859° S |
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
Authenticating...
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