QIANFAN-42, 62243
Orbit data source: Space-Track
QIANFAN-42, 62243 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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62243 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Partially 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: 18 hours ago
TLE from 18 hours ago
0 QIANFAN-42
1 62243U 24232G 26306.84633887 .00000213 00000-0 85265-4 0 9990
2 62243 89.0116 0.4422 0017314 100.7559 259.5584 14.24675700147656Epoch: 2026-11-02T20:18Z
TLE epoch observation values (Epoch: 2026-11-02T20:18:43.678Z)
Latitude
-0.00001°
Longitude
13.64271°
Altitude
814.92 km
Speed
7.445 km/s
True Right ascension
00h 01m 46s
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
10:39:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
818.967 km
Perigee altitude
794.088 km
Semi-major axis
7,184.665 km
Eccentricity
0.00173
Inclination
89.0116°
RAAN
0.4422°
Arg. of periapsis
100.7559°
True anomaly
259.36336°
Mean anomaly
259.5584°
Eccentric anomaly
259.46087°
Mean motion
3.56396 °/min
Orbital period
101.01 mins
BSTAR
0.000085265
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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-42 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 | 2026-11-03 15:25:33.734Z | 16.205° NNE | 2026-11-03 15:30:33.734Z | 88.278° E | 40.691° | 2026-11-03 15:34:33.734Z | 151.312° SSE |
| 6 mins | 2026-11-03 17:08:33.734Z | 320.239° NNW | 2026-11-03 17:11:33.734Z | 276.862° WNW | 22.433° | 2026-11-03 17:14:33.734Z | 238.063° WSW |
| 4 mins | 2026-11-04 02:49:33.734Z | 94.111° ESE | 2026-11-04 02:50:33.734Z | 81.335° E | 15.99° | 2026-11-04 02:53:33.734Z | 44.206° NE |
| 9 mins | 2026-11-04 04:27:33.734Z | 196.027° SSW | 2026-11-04 04:31:33.734Z | 272.691° WNW | 58.228° | 2026-11-04 04:36:33.734Z | 350.416° N |
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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