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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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: 5 hours ago
TLE from 5 hours ago
0 QIANFAN-37
1 62238U 24232B 25288.62969686 .00000169 00000-0 24273-3 0 9998
2 62238 89.0017 47.1828 0001174 114.2922 245.8352 13.50971033 91328Epoch: 2025-10-15T15:06Z
TLE epoch observation values (Epoch: 2025-10-15T15:06:45.808Z)
Latitude
-0.00002°
Longitude
156.09091°
Altitude
1,071.999 km
Speed
7.316 km/s
True Right ascension
03h 08m 43s
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
14:54:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,066.613 km
Perigee altitude
1,064.865 km
Semi-major axis
7,443.876 km
Eccentricity
0.00012
Inclination
89.0017°
RAAN
47.1828°
Arg. of periapsis
114.2922°
True anomaly
245.82293°
Mean anomaly
245.8352°
Eccentric anomaly
245.82906°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.00024273
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-10-15 21:02:37.880Z | 345.003° N | 2025-10-15 21:07:37.880Z | 286.896° WNW | 34.899° | 2025-10-15 21:13:37.880Z | 210.655° SW |
| 8 mins | 2025-10-16 07:15:37.880Z | 115.853° SE | 2025-10-16 07:18:37.880Z | 81.399° E | 23.054° | 2025-10-16 07:23:37.880Z | 27.396° NE |
| 10 mins | 2025-10-16 09:00:37.880Z | 205.255° SW | 2025-10-16 09:04:37.880Z | 259.047° W | 37.436° | 2025-10-16 09:10:37.880Z | 345.997° N |
| 7 mins | 2025-10-16 20:09:37.880Z | 4.907° NNE | 2025-10-16 20:14:37.880Z | 83.892° E | 44.462° | 2025-10-16 20:16:37.880Z | 167.333° 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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