QIANFAN-37, 62238
Orbit data source: Space-Track
QIANFAN-37, 62238 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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62238 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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-37
1 62238U 24232B 26246.84178101 .00000093 00000-0 12533-3 0 9993
2 62238 89.0136 14.6985 0002360 90.1138 270.0283 13.51028070134968Epoch: 2026-09-03T20:12Z
TLE epoch observation values (Epoch: 2026-09-03T20:12:09.879Z)
Latitude
-0.00007°
Longitude
88.68317°
Altitude
1,071.431 km
Speed
7.316 km/s
True Right ascension
00h 58m 47s
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
20:54:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,067.286 km
Perigee altitude
1,063.773 km
Semi-major axis
7,443.666 km
Eccentricity
0.00024
Inclination
89.0136°
RAAN
14.6985°
Arg. of periapsis
90.1138°
True anomaly
270.00126°
Mean anomaly
270.0283°
Eccentric anomaly
270.01478°
Mean motion
3.37958 °/min
Orbital period
106.52 mins
BSTAR
0.00012533
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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-37 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-09-04 08:44:51.439Z | 164.705° S | 2026-09-04 08:50:51.439Z | 68.728° E | 42.47° | 2026-09-04 08:56:51.439Z | 5.022° NNE |
| 7 mins | 2026-09-04 10:34:51.439Z | 253.197° W | 2026-09-04 10:37:51.439Z | 285.402° WNW | 17.926° | 2026-09-04 10:41:51.439Z | 324.199° NNW |
| 9 mins | 2026-09-04 19:55:51.439Z | 31.203° NE | 2026-09-04 19:59:51.439Z | 81.934° E | 27.9° | 2026-09-04 20:04:51.439Z | 139.532° SSE |
| 10 mins | 2026-09-04 21:41:51.439Z | 339.393° N | 2026-09-04 21:46:51.439Z | 270.407° WNW | 32.469° | 2026-09-04 21:51:51.439Z | 215.463° SW |
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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