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.
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
62249 intel report (Beta)
Focus sentinelFocus sentinel
Create New Watchlist
Focus sentinelFocus sentinel
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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-48
1 62249U 24232N 25261.97465647 .00000080 00000-0 10482-3 0 9996
2 62249 88.9979 49.7651 0018962 86.7355 273.5965 13.50967615 87800Epoch: 2025-09-18T23:23Z
TLE epoch observation values (Epoch: 2025-09-18T23:23:30.319Z)
Latitude
-0.00001°
Longitude
60.76022°
Altitude
1,070.795 km
Speed
7.317 km/s
True Right ascension
03h 19m 03s
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
01:35:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,079.867 km
Perigee altitude
1,051.637 km
Semi-major axis
7,443.889 km
Eccentricity
0.0019
Inclination
88.9979°
RAAN
49.7651°
Arg. of periapsis
86.7355°
True anomaly
273.37961°
Mean anomaly
273.5965°
Eccentric anomaly
273.48806°
Mean motion
3.37943 °/min
Orbital period
106.53 mins
BSTAR
0.00010482
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #232 in the year 2024 (2024-12-05 UTC)
Did you know?
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
Loading observer location...
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 | 2025-09-19 10:09:17.526Z | 168.279° S | 2025-09-19 10:15:17.526Z | 82.106° E | 43.667° | 2025-09-19 10:21:17.526Z | 3.772° NNE |
| 6 mins | 2025-09-19 12:00:17.526Z | 261.308° W | 2025-09-19 12:02:17.526Z | 282.379° WNW | 16.394° | 2025-09-19 12:06:17.526Z | 321.25° NNW |
| 10 mins | 2025-09-19 21:20:17.526Z | 27.873° NE | 2025-09-19 21:24:17.526Z | 78.102° E | 29.494° | 2025-09-19 21:30:17.526Z | 146.236° SSE |
| 10 mins | 2025-09-19 23:06:17.526Z | 338.817° N | 2025-09-19 23:11:17.526Z | 275.303° WNW | 30.735° | 2025-09-19 23:16:17.526Z | 219.087° SW |
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 ascending order |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
|---|