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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-53
1 62254U 24232T 26246.85421776 .00000075 00000-0 96717-4 0 9998
2 62254 89.0145 14.6080 0015620 142.6287 217.5953 13.51025394103707Epoch: 2026-09-03T20:30Z
TLE epoch observation values (Epoch: 2026-09-03T20:30:04.414Z)
Latitude
-0.0001°
Longitude
84.10318°
Altitude
1,080.666 km
Speed
7.307 km/s
True Right ascension
00h 58m 25s
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
20:54:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.166 km
Perigee altitude
1,053.912 km
Semi-major axis
7,443.676 km
Eccentricity
0.00156
Inclination
89.0145°
RAAN
14.608°
Arg. of periapsis
142.6287°
True anomaly
217.48627°
Mean anomaly
217.5953°
Eccentric anomaly
217.54077°
Mean motion
3.37957 °/min
Orbital period
106.52 mins
BSTAR
0.000096717
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-04 07:20:09.507Z | 95.849° ESE | 2026-09-04 07:23:09.507Z | 67.901° E | 13.311° | 2026-09-04 07:25:09.507Z | 49.128° ENE |
| 11 mins | 2026-09-04 09:03:09.507Z | 177.629° S | 2026-09-04 09:08:09.507Z | 183.63° SSW | 44.822° | 2026-09-04 09:14:09.507Z | 358.885° N |
| 4 mins | 2026-09-04 10:54:09.507Z | 270.1° WNW | 2026-09-04 10:56:09.507Z | 289.134° WNW | 12.766° | 2026-09-04 10:58:09.507Z | 307.659° NW |
| 10 mins | 2026-09-04 20:13:09.507Z | 20.3° NNE | 2026-09-04 20:18:09.507Z | 91.949° ESE | 34.609° | 2026-09-04 20:23:09.507Z | 152.725° SSE |
| 9 mins | 2026-09-04 22:00:09.507Z | 330.092° NNW | 2026-09-04 22:04:09.507Z | 282.038° WNW | 25.747° | 2026-09-04 22:09:09.507Z | 228.133° WSW |
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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