QIANFAN-49, 62250
Orbit data source: Space-Track
QIANFAN-49, 62250 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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62250 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: 4 hours ago
TLE from 4 hours ago
0 QIANFAN-49
1 62250U 24232P 25342.61857265 .00000184 00000-0 26626-3 0 9992
2 62250 89.0031 41.6517 0013891 199.1042 160.9590 13.50978066 67288Epoch: 2025-12-08T14:50Z
TLE epoch observation values (Epoch: 2025-12-08T14:50:44.676Z)
Latitude
-0.00004°
Longitude
101.35053°
Altitude
1,081.397 km
Speed
7.307 km/s
True Right ascension
02h 46m 36s
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
17:23:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.053 km
Perigee altitude
1,055.373 km
Semi-major axis
7,443.85 km
Eccentricity
0.00139
Inclination
89.0031°
RAAN
41.6517°
Arg. of periapsis
199.1042°
True anomaly
161.01085°
Mean anomaly
160.959°
Eccentric anomaly
160.98493°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.00026626
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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-49 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 | 2025-12-09 03:24:36.771Z | 130.065° SE | 2025-12-09 03:29:36.771Z | 77.473° E | 25.054° | 2025-12-09 03:34:36.771Z | 24.37° NE |
| 11 mins | 2025-12-09 05:10:36.771Z | 205.604° SW | 2025-12-09 05:15:36.771Z | 268.331° W | 36.001° | 2025-12-09 05:21:36.771Z | 345.19° N |
| 11 mins | 2025-12-09 16:20:36.771Z | 2.73° NNE | 2025-12-09 16:25:36.771Z | 139.401° SSE | 44.815° | 2025-12-09 16:31:36.771Z | 180.662° SSW |
| 4 mins | 2025-12-09 18:09:36.771Z | 302.786° NW | 2025-12-09 18:10:36.771Z | 292.903° NW | 13.906° | 2025-12-09 18:13:36.771Z | 264.08° 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
Authenticating...
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