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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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-49
1 62250U 24232P 26305.19836287 .00000085 00000-0 11248-3 0 9990
2 62250 89.0158 8.8192 0013169 348.2922 11.7921 13.51034767111513Epoch: 2026-11-01T04:45Z
TLE epoch observation values (Epoch: 2026-11-01T04:45:38.551Z)
Latitude
-0.00005°
Longitude
-103.08461°
Altitude
1,061.806 km
Speed
7.326 km/s
True Right ascension
00h 35m 16s
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
06:21:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.307 km
Perigee altitude
1,055.702 km
Semi-major axis
7,443.642 km
Eccentricity
0.00132
Inclination
89.0158°
RAAN
8.8192°
Arg. of periapsis
348.2922°
True anomaly
11.82299°
Mean anomaly
11.7921°
Eccentric anomaly
11.80754°
Mean motion
3.3796 °/min
Orbital period
106.52 mins
BSTAR
0.00011248
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-11-01 16:00:58.654Z | 15.033° NNE | 2026-11-01 16:06:58.654Z | 85.926° E | 44.427° | 2026-11-01 16:12:58.654Z | 155.546° SSE |
| 9 mins | 2026-11-01 17:48:58.654Z | 331.629° NNW | 2026-11-01 17:52:58.654Z | 285.837° WNW | 29.356° | 2026-11-01 17:57:58.654Z | 229.716° WSW |
| 10 mins | 2026-11-02 03:59:58.654Z | 136.525° SSE | 2026-11-02 04:03:58.654Z | 82.666° E | 38.668° | 2026-11-02 04:09:58.654Z | 15.273° NNE |
| 10 mins | 2026-11-02 05:45:58.654Z | 221.375° SW | 2026-11-02 05:50:58.654Z | 283.697° WNW | 32.779° | 2026-11-02 05:55:58.654Z | 337.659° 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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