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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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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-52
1 62253U 24232S 26246.87475473 .00000090 00000-0 11983-3 0 9990
2 62253 89.0138 14.4814 0016759 141.8563 218.3778 13.51028537103743Epoch: 2026-09-03T20:59Z
TLE epoch observation values (Epoch: 2026-09-03T20:59:38.808Z)
Latitude
-0.00001°
Longitude
76.56304°
Altitude
1,081.223 km
Speed
7.307 km/s
True Right ascension
00h 57m 55s
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
20:52:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.002 km
Perigee altitude
1,053.053 km
Semi-major axis
7,443.665 km
Eccentricity
0.00168
Inclination
89.0138°
RAAN
14.4814°
Arg. of periapsis
141.8563°
True anomaly
218.25877°
Mean anomaly
218.3778°
Eccentric anomaly
218.31826°
Mean motion
3.37958 °/min
Orbital period
106.52 mins
BSTAR
0.00011983
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-09-04 07:46:59.078Z | 125.63° SE | 2026-09-04 07:51:59.078Z | 75.379° E | 22.263° | 2026-09-04 07:56:59.078Z | 25.535° NE |
| 11 mins | 2026-09-04 09:32:59.078Z | 200.814° SSW | 2026-09-04 09:37:59.078Z | 271.85° WNW | 38.818° | 2026-09-04 09:43:59.078Z | 348.375° N |
| 12 mins | 2026-09-04 20:41:59.078Z | 5.508° NNE | 2026-09-04 20:47:59.078Z | 126.283° SE | 43.517° | 2026-09-04 20:53:59.078Z | 175.683° S |
| 6 mins | 2026-09-04 22:30:59.078Z | 311.044° NW | 2026-09-04 22:32:59.078Z | 290.477° WNW | 16.02° | 2026-09-04 22:36:59.078Z | 251.831° W |
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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