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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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 26304.12107995 .00000142 00000-0 20133-3 0 9998
2 61562 88.9866 48.0160 0009801 187.7460 172.3541 13.51108331111324Epoch: 2026-10-31T02:54Z
TLE epoch observation values (Epoch: 2026-10-31T02:54:21.307Z)
Latitude
-0.00007°
Longitude
-35.00413°
Altitude
1,078.372 km
Speed
7.309 km/s
True Right ascension
03h 12m 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
06:34:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,072.53 km
Perigee altitude
1,057.939 km
Semi-major axis
7,443.371 km
Eccentricity
0.00098
Inclination
88.9866°
RAAN
48.016°
Arg. of periapsis
187.746°
True anomaly
172.36902°
Mean anomaly
172.3541°
Eccentric anomaly
172.36156°
Mean motion
3.37978 °/min
Orbital period
106.52 mins
BSTAR
0.00020133
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-31 17:45:20.226Z | 46.086° ENE | 2026-10-31 17:48:20.226Z | 74.972° E | 15.378° | 2026-10-31 17:51:20.226Z | 103.969° ESE |
| 11 mins | 2026-10-31 19:30:20.226Z | 357.857° N | 2026-10-31 19:35:20.226Z | 308.813° NW | 78.216° | 2026-10-31 19:41:20.226Z | 187.844° SSW |
| 4 mins | 2026-11-01 05:45:20.226Z | 85.455° E | 2026-11-01 05:47:20.226Z | 66.275° ENE | 13.5° | 2026-11-01 05:49:20.226Z | 47.885° ENE |
| 11 mins | 2026-11-01 07:27:20.226Z | 176.886° S | 2026-11-01 07:32:20.226Z | 158.853° S | 87.714° | 2026-11-01 07:38:20.226Z | 359.336° N |
| 4 mins | 2026-11-01 09:18:20.226Z | 271.674° WNW | 2026-11-01 09:20:20.226Z | 290.938° WNW | 13.476° | 2026-11-01 09:22:20.226Z | 309.342° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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