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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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: 13 hours ago
TLE from 13 hours ago
0 QIANFAN-34
1 61567U 24185R 25286.64320344 .00000597 00000-0 38123-3 0 9995
2 61567 88.9723 85.1484 0007037 143.5508 216.6152 14.02224090 60932Epoch: 2025-10-13T15:26Z
TLE epoch observation values (Epoch: 2025-10-13T15:26:12.777Z)
Latitude
-0.00005°
Longitude
-168.84788°
Altitude
893.236 km
Speed
7.403 km/s
True Right ascension
05h 40m 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
22:30:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
888.19 km
Perigee altitude
877.971 km
Semi-major axis
7,261.218 km
Eccentricity
0.0007
Inclination
88.9723°
RAAN
85.1484°
Arg. of periapsis
143.5508°
True anomaly
216.56714°
Mean anomaly
216.6152°
Eccentric anomaly
216.59117°
Mean motion
3.50775 °/min
Orbital period
102.63 mins
BSTAR
0.00038123
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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 | 2025-10-14 10:23:07.288Z | 146.263° SSE | 2025-10-14 10:28:07.288Z | 81.724° E | 31.545° | 2025-10-14 10:33:07.288Z | 16.574° NNE |
| 8 mins | 2025-10-14 12:07:07.288Z | 228.036° WSW | 2025-10-14 12:11:07.288Z | 282.564° WNW | 24.58° | 2025-10-14 12:15:07.288Z | 331.801° NNW |
| 10 mins | 2025-10-14 22:51:07.288Z | 4.05° NNE | 2025-10-14 22:56:07.288Z | 133.677° SE | 44.215° | 2025-10-14 23:01:07.288Z | 177.965° S |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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