QIANFAN-34, 61567
Orbit data source: Space-Track
QIANFAN-34, 61567 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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61567 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GESIH/SECM
Mission
Partially 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: 15 hours ago
TLE from 15 hours ago
0 QIANFAN-34
1 61567U 24185R 26235.58984639 .00000265 00000-0 16315-3 0 9997
2 61567 88.9769 49.7332 0004357 243.7808 116.2925 14.02503493104937Epoch: 2026-08-23T14:09Z
TLE epoch observation values (Epoch: 2026-08-23T14:09:22.728Z)
Latitude
0.00004°
Longitude
-134.49522°
Altitude
889.57 km
Speed
7.407 km/s
True Right ascension
03h 18m 55s
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
20:47:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
885.279 km
Perigee altitude
878.952 km
Semi-major axis
7,260.252 km
Eccentricity
0.00044
Inclination
88.9769°
RAAN
49.7332°
Arg. of periapsis
243.7808°
True anomaly
116.33725°
Mean anomaly
116.2925°
Eccentric anomaly
116.31488°
Mean motion
3.50845 °/min
Orbital period
102.61 mins
BSTAR
0.00016315
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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-34 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-24 10:50:26.263Z | 117.866° SE | 2026-08-24 10:54:26.263Z | 72.247° E | 18.271° | 2026-08-24 10:57:26.263Z | 37.538° NE |
| 9 mins | 2026-08-24 12:32:26.263Z | 200.779° SSW | 2026-08-24 12:36:26.263Z | 276.206° WNW | 39.197° | 2026-08-24 12:41:26.263Z | 348.445° N |
| 9 mins | 2026-08-24 23:17:26.263Z | 24.25° NE | 2026-08-24 23:21:26.263Z | 88.612° E | 32.42° | 2026-08-24 23:26:26.263Z | 152.984° SSE |
| 7 mins | 2026-08-25 01:00:26.263Z | 326.22° NNW | 2026-08-25 01:03:26.263Z | 286.321° WNW | 23.802° | 2026-08-25 01:07:26.263Z | 233.426° 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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