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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Edit Public Description
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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-42
1 62243U 24232G 25312.14109861 .00000875 00000-0 37180-3 0 9995
2 62243 89.0036 41.3014 0014939 189.3534 170.7383 14.24431399 96449Epoch: 2025-11-08T03:23Z
TLE epoch observation values (Epoch: 2025-11-08T03:23:10.919Z)
Latitude
-0.00002°
Longitude
-57.06907°
Altitude
824.066 km
Speed
7.435 km/s
True Right ascension
02h 45m 12s
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
06:14:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
818.084 km
Perigee altitude
796.615 km
Semi-major axis
7,185.487 km
Eccentricity
0.00149
Inclination
89.0036°
RAAN
41.3014°
Arg. of periapsis
189.3534°
True anomaly
170.7658°
Mean anomaly
170.7383°
Eccentric anomaly
170.75206°
Mean motion
3.56335 °/min
Orbital period
101.03 mins
BSTAR
0.0003718
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-08 17:27:46.263Z | 29.816° NE | 2025-11-08 17:31:46.263Z | 84.611° E | 23.688° | 2025-11-08 17:35:46.263Z | 136.695° SSE |
| 7 mins | 2025-11-08 19:09:46.263Z | 330.728° NNW | 2025-11-08 19:12:46.263Z | 278.355° WNW | 29.757° | 2025-11-08 19:16:46.263Z | 218.884° SW |
| 9 mins | 2025-11-09 06:28:46.263Z | 176.879° S | 2025-11-09 06:32:46.263Z | 161.97° S | 44.895° | 2025-11-09 06:37:46.263Z | 359.439° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
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