QIANFAN-29, 61562
Orbit data source: Space-Track
QIANFAN-29, 61562 is a Chinese payload satellite in LEO that was launched on Tue, 15 Oct 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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61562 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GESIH/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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-29
1 61562U 24185L 26034.10090192 .00000199 00000-0 29009-3 0 9999
2 61562 88.9734 75.8988 0007958 255.1968 104.8302 13.51031828 74866Epoch: 2026-02-03T02:25Z
TLE epoch observation values (Epoch: 2026-02-03T02:25:17.925Z)
Latitude
-0.00002°
Longitude
-93.71256°
Altitude
1,072.939 km
Speed
7.315 km/s
True Right ascension
05h 03m 35s
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
12:05:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,071.439 km
Perigee altitude
1,059.592 km
Semi-major axis
7,443.653 km
Eccentricity
0.0008
Inclination
88.9734°
RAAN
75.8988°
Arg. of periapsis
255.1968°
True anomaly
104.91833°
Mean anomaly
104.8302°
Eccentric anomaly
104.87427°
Mean motion
3.37959 °/min
Orbital period
106.52 mins
BSTAR
0.00029009
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Other satellites on launch #185 in the year 2024 (2024-10-15 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-29 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-02-03 13:41:45.007Z | 31.602° NE | 2026-02-03 13:46:45.007Z | 84.251° E | 21.189° | 2026-02-03 13:50:45.007Z | 124.998° SE |
| 10 mins | 2026-02-03 15:28:45.007Z | 346.54° N | 2026-02-03 15:32:45.007Z | 293.34° NW | 39.226° | 2026-02-03 15:38:45.007Z | 202.763° SW |
| 8 mins | 2026-02-04 01:40:45.007Z | 110.726° ESE | 2026-02-04 01:44:45.007Z | 68.555° E | 18.937° | 2026-02-04 01:48:45.007Z | 30.756° NE |
| 12 mins | 2026-02-04 03:24:45.007Z | 192.247° SSW | 2026-02-04 03:29:45.007Z | 251.039° W | 41.657° | 2026-02-04 03:36:45.007Z | 353.016° N |
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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