QIANFAN-52, 62253
Orbit data source: Space-Track
QIANFAN-52, 62253 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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62253 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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-52
1 62253U 24232S 26035.12951093 .00000011 00000-0 -10724-5 0 9999
2 62253 89.0005 35.7147 0016682 43.5055 316.7409 13.50994657 75151Epoch: 2026-02-04T03:06Z
TLE epoch observation values (Epoch: 2026-02-04T03:06:29.744Z)
Latitude
0°
Longitude
-145.20975°
Altitude
1,062.515 km
Speed
7.325 km/s
True Right ascension
02h 22m 51s
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
10:40:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.07 km
Perigee altitude
1,053.235 km
Semi-major axis
7,443.789 km
Eccentricity
0.00167
Inclination
89.0005°
RAAN
35.7147°
Arg. of periapsis
43.5055°
True anomaly
316.6097°
Mean anomaly
316.7409°
Eccentric anomaly
316.67532°
Mean motion
3.3795 °/min
Orbital period
106.52 mins
BSTAR
-0.0000010724
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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-52 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 | 2026-02-04 10:50:19.967Z | 39.619° NE | 2026-02-04 10:54:19.967Z | 81.358° E | 18.614° | 2026-02-04 10:58:19.967Z | 120.24° SE |
| 11 mins | 2026-02-04 12:36:19.967Z | 351.163° N | 2026-02-04 12:41:19.967Z | 261.264° W | 41.947° | 2026-02-04 12:47:19.967Z | 195.801° SSW |
| 5 mins | 2026-02-04 22:50:19.967Z | 93.549° ESE | 2026-02-04 22:52:19.967Z | 72.324° E | 16.408° | 2026-02-04 22:55:19.967Z | 42.152° NE |
| 11 mins | 2026-02-05 00:33:19.967Z | 187.679° SSW | 2026-02-05 00:38:19.967Z | 291.272° WNW | 43.623° | 2026-02-05 00:44:19.967Z | 355.056° 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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