QIANFAN-53, 62254
Orbit data source: Space-Track
QIANFAN-53, 62254 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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62254 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-53
1 62254U 24232T 26096.87749439 .00000169 00000-0 24249-3 0 9996
2 62254 89.0111 29.6206 0012475 215.2412 144.7915 13.51010084 83456Epoch: 2026-04-06T21:03Z
TLE epoch observation values (Epoch: 2026-04-06T21:03:35.515Z)
Latitude
-0.00006°
Longitude
-121.43964°
Altitude
1,079.093 km
Speed
7.309 km/s
True Right ascension
01h 58m 28s
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
14:02:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.882 km
Perigee altitude
1,056.309 km
Semi-major axis
7,443.732 km
Eccentricity
0.00125
Inclination
89.0111°
RAAN
29.6206°
Arg. of periapsis
215.2412°
True anomaly
144.87382°
Mean anomaly
144.7915°
Eccentric anomaly
144.83267°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.00024249
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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-53 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 | 2026-04-07 08:19:29.390Z | 348.226° N | 2026-04-07 08:24:29.390Z | 289.229° WNW | 38.051° | 2026-04-07 08:30:29.390Z | 205.066° SW |
| 8 mins | 2026-04-07 18:32:29.390Z | 111.676° ESE | 2026-04-07 18:35:29.390Z | 80.001° E | 20.285° | 2026-04-07 18:40:29.390Z | 29.378° NE |
| 11 mins | 2026-04-07 20:16:29.390Z | 195.266° SSW | 2026-04-07 20:21:29.390Z | 256.692° W | 40.601° | 2026-04-07 20:27:29.390Z | 349.493° N |
| 11 mins | 2026-04-08 07:26:29.390Z | 9.135° NNE | 2026-04-08 07:31:29.390Z | 89.461° E | 42.791° | 2026-04-08 07:37:29.390Z | 171.127° 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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