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: 12 hours ago
TLE from 12 hours ago
0 QIANFAN-49
1 62250U 24232P 25259.51815923 .00000091 00000-0 12229-3 0 9994
2 62250 88.9972 50.0272 0016076 88.3491 271.9501 13.50960043 56062Epoch: 2025-09-16T12:26Z
TLE epoch observation values (Epoch: 2025-09-16T12:26:08.957Z)
Latitude
-0.00006°
Longitude
-132.21743°
Altitude
1,071.293 km
Speed
7.317 km/s
True Right ascension
03h 20m 06s
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
17:28:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.746 km
Perigee altitude
1,053.813 km
Semi-major axis
7,443.917 km
Eccentricity
0.00161
Inclination
88.9972°
RAAN
50.0272°
Arg. of periapsis
88.3491°
True anomaly
271.76598°
Mean anomaly
271.9501°
Eccentric anomaly
271.85804°
Mean motion
3.37941 °/min
Orbital period
106.53 mins
BSTAR
0.00012229
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-09-17 09:52:09.717Z | 150.91° SSE | 2025-09-17 09:58:09.717Z | 76.964° E | 35.518° | 2025-09-17 10:03:09.717Z | 15.037° NNE |
| 8 mins | 2025-09-17 11:41:09.717Z | 235.555° WSW | 2025-09-17 11:45:09.717Z | 286.44° WNW | 24.746° | 2025-09-17 11:49:09.717Z | 330.113° NNW |
| 8 mins | 2025-09-17 21:03:09.717Z | 38.204° NE | 2025-09-17 21:07:09.717Z | 81.819° E | 20.295° | 2025-09-17 21:11:09.717Z | 122.74° SE |
| 11 mins | 2025-09-17 22:49:09.717Z | 348.447° N | 2025-09-17 22:54:09.717Z | 263.726° W | 40.192° | 2025-09-17 23:00:09.717Z | 199.286° SSW |
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 |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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