QIANFAN-48, 62249
Orbit data source: Space-Track
QIANFAN-48, 62249 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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62249 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: 11 hours ago
TLE from 11 hours ago
0 QIANFAN-48
1 62249U 24232N 26096.87337999 .00000174 00000-0 25124-3 0 9993
2 62249 89.0109 29.6259 0015190 224.1883 135.8055 13.51009954114795Epoch: 2026-04-06T20:57Z
TLE epoch observation values (Epoch: 2026-04-06T20:57:40.031Z)
Latitude
-0.00008°
Longitude
-119.9491°
Altitude
1,079.618 km
Speed
7.308 km/s
True Right ascension
01h 58m 30s
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
14:00:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.903 km
Perigee altitude
1,054.289 km
Semi-major axis
7,443.733 km
Eccentricity
0.00152
Inclination
89.0109°
RAAN
29.6259°
Arg. of periapsis
224.1883°
True anomaly
135.92667°
Mean anomaly
135.8055°
Eccentric anomaly
135.8661°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.00025124
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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-48 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 | 2026-04-07 08:13:24.158Z | 350.948° N | 2026-04-07 08:19:24.158Z | 261.441° W | 40.023° | 2026-04-07 08:25:24.158Z | 199.389° SSW |
| 7 mins | 2026-04-07 18:27:24.158Z | 102.546° ESE | 2026-04-07 18:30:24.158Z | 70.009° E | 18.544° | 2026-04-07 18:34:24.158Z | 31.969° NE |
| 12 mins | 2026-04-07 20:10:24.158Z | 190.631° SSW | 2026-04-07 20:16:24.158Z | 294.684° NW | 42.103° | 2026-04-07 20:22:24.158Z | 353.325° N |
| 11 mins | 2026-04-08 07:20:24.158Z | 11.236° NNE | 2026-04-08 07:25:24.158Z | 80.764° E | 41.126° | 2026-04-08 07:31:24.158Z | 166.781° S |
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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