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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-34
1 61567U 24185R 26171.44940220 .00000272 00000-0 16807-3 0 9993
2 61567 88.9792 56.9679 0008453 91.7572 268.4576 14.02470581 95940Epoch: 2026-06-20T10:47Z
TLE epoch observation values (Epoch: 2026-06-20T10:47:08.350Z)
Latitude
-0.00005°
Longitude
-13.48076°
Altitude
888.451 km
Speed
7.408 km/s
True Right ascension
03h 47m 52s
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
07:24:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
888.366 km
Perigee altitude
876.092 km
Semi-major axis
7,260.366 km
Eccentricity
0.00085
Inclination
88.9792°
RAAN
56.9679°
Arg. of periapsis
91.7572°
True anomaly
268.36077°
Mean anomaly
268.4576°
Eccentric anomaly
268.40919°
Mean motion
3.50837 °/min
Orbital period
102.61 mins
BSTAR
0.00016807
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-06-21 04:29:16.242Z | 6.196° NNE | 2026-06-21 04:34:16.242Z | 75.709° E | 43.254° | 2026-06-21 04:39:16.242Z | 172.594° S |
| 4 mins | 2026-06-21 06:15:16.242Z | 299.741° NW | 2026-06-21 06:16:16.242Z | 288.02° WNW | 14.285° | 2026-06-21 06:19:16.242Z | 255.453° W |
| 9 mins | 2026-06-21 16:01:16.242Z | 138.855° SSE | 2026-06-21 16:05:16.242Z | 81.819° E | 30.004° | 2026-06-21 16:10:16.242Z | 17.735° NNE |
| 8 mins | 2026-06-21 17:44:16.242Z | 226.147° WSW | 2026-06-21 17:48:16.242Z | 283.066° WNW | 25.759° | 2026-06-21 17:52:16.242Z | 333.13° NNW |
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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