QIANFAN-51, 62252
Orbit data source: Space-Track
QIANFAN-51, 62252 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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62252 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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-51
1 62252U 24232R 25287.89315744 .00000155 00000-0 22081-3 0 9992
2 62252 89.0022 47.1623 0013371 18.1039 342.0586 13.50976175 59916Epoch: 2025-10-14T21:26Z
TLE epoch observation values (Epoch: 2025-10-14T21:26:08.802Z)
Latitude
-0°
Longitude
61.95057°
Altitude
1,062.149 km
Speed
7.325 km/s
True Right ascension
03h 08m 38s
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
02:16:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.673 km
Perigee altitude
1,055.767 km
Semi-major axis
7,443.857 km
Eccentricity
0.00134
Inclination
89.0022°
RAAN
47.1623°
Arg. of periapsis
18.1039°
True anomaly
342.01133°
Mean anomaly
342.0586°
Eccentric anomaly
342.03497°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.00022081
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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-51 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 | 2025-10-15 08:11:35.902Z | 165.592° S | 2025-10-15 08:17:35.902Z | 101.04° ESE | 42.432° | 2025-10-15 08:23:35.902Z | 5.892° NNE |
| 7 mins | 2025-10-15 10:01:35.902Z | 247.988° W | 2025-10-15 10:04:35.902Z | 278.563° WNW | 17.771° | 2025-10-15 10:08:35.902Z | 319.821° NNW |
| 10 mins | 2025-10-15 19:22:35.902Z | 27.066° NE | 2025-10-15 19:27:35.902Z | 88.63° E | 27.884° | 2025-10-15 19:32:35.902Z | 141.633° SSE |
| 10 mins | 2025-10-15 21:09:35.902Z | 337.07° NNW | 2025-10-15 21:13:35.902Z | 283.461° WNW | 32.742° | 2025-10-15 21:19:35.902Z | 213.954° SW |
| 9 mins | 2025-10-16 07:20:35.902Z | 125.73° SE | 2025-10-16 07:24:35.902Z | 80.256° E | 25.144° | 2025-10-16 07:29:35.902Z | 24.946° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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