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 26035.17063146 .00000052 00000-0 61393-4 0 9991
2 62238 89.0003 35.9277 0001489 73.6055 286.5259 13.50996990106380Epoch: 2026-02-04T04:05Z
TLE epoch observation values (Epoch: 2026-02-04T04:05:42.558Z)
Latitude
-0.00008°
Longitude
-159.84068°
Altitude
1,071.231 km
Speed
7.317 km/s
True Right ascension
02h 23m 42s
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
10:44:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,066.752 km
Perigee altitude
1,064.535 km
Semi-major axis
7,443.781 km
Eccentricity
0.00015
Inclination
89.0003°
RAAN
35.9277°
Arg. of periapsis
73.6055°
True anomaly
286.50954°
Mean anomaly
286.5259°
Eccentric anomaly
286.51772°
Mean motion
3.3795 °/min
Orbital period
106.52 mins
BSTAR
0.000061393
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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 | 2026-02-04 11:48:05.954Z | 11.718° NNE | 2026-02-04 11:54:05.954Z | 99.361° ESE | 39.382° | 2026-02-04 12:00:05.954Z | 164.68° S |
| 8 mins | 2026-02-04 13:36:05.954Z | 325.036° NNW | 2026-02-04 13:40:05.954Z | 280.512° WNW | 21.391° | 2026-02-04 13:44:05.954Z | 239.676° WSW |
| 11 mins | 2026-02-04 23:46:05.954Z | 149.111° SSE | 2026-02-04 23:51:05.954Z | 74.908° E | 36.838° | 2026-02-04 23:57:05.954Z | 10.51° NNE |
| 8 mins | 2026-02-05 01:34:05.954Z | 237.779° WSW | 2026-02-05 01:37:05.954Z | 272.618° WNW | 23.652° | 2026-02-05 01:42:05.954Z | 329.358° NNW |
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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