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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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: 4 hours ago
TLE from 4 hours ago
0 QIANFAN-39
1 62240U 24232D 26050.50037853 .00000233 00000-0 92745-4 0 9990
2 62240 89.0032 29.4376 0014785 206.4111 153.6330 14.25425573111180Epoch: 2026-02-19T12:00Z
TLE epoch observation values (Epoch: 2026-02-19T12:00:32.704Z)
Latitude
-0.00007°
Longitude
59.85056°
Altitude
819.646 km
Speed
7.438 km/s
True Right ascension
01h 57m 45s
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
19:16:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
814.624 km
Perigee altitude
793.387 km
Semi-major axis
7,182.143 km
Eccentricity
0.00148
Inclination
89.0032°
RAAN
29.4376°
Arg. of periapsis
206.4111°
True anomaly
153.70812°
Mean anomaly
153.633°
Eccentric anomaly
153.67057°
Mean motion
3.56584 °/min
Orbital period
100.96 mins
BSTAR
0.000092745
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-02-19 22:14:38.670Z | 140.066° SSE | 2026-02-19 22:18:38.670Z | 77.511° E | 30.104° | 2026-02-19 22:22:38.670Z | 20.57° NNE |
| 7 mins | 2026-02-19 23:56:38.670Z | 234.143° WSW | 2026-02-19 23:59:38.670Z | 279.826° WNW | 23.937° | 2026-02-20 00:03:38.670Z | 331.771° NNW |
| 8 mins | 2026-02-20 10:30:38.670Z | 14.629° NNE | 2026-02-20 10:33:38.670Z | 67.301° ENE | 40.362° | 2026-02-20 10:38:38.670Z | 167.269° S |
| 4 mins | 2026-02-20 12:12:38.670Z | 308.208° NW | 2026-02-20 12:14:38.670Z | 282.976° WNW | 15.01° | 2026-02-20 12:16:38.670Z | 258.485° W |
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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