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
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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-34
1 61567U 24185R 26071.98857808 .00000558 00000-0 35493-3 0 9999
2 61567 88.9721 68.1681 0007964 58.2072 301.9883 14.02391021 82007Epoch: 2026-03-12T23:43Z
TLE epoch observation values (Epoch: 2026-03-12T23:43:33.146Z)
Latitude
0.00001°
Longitude
-98.35057°
Altitude
885.493 km
Speed
7.411 km/s
True Right ascension
04h 32m 40s
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
10:48:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
888.286 km
Perigee altitude
876.722 km
Semi-major axis
7,260.641 km
Eccentricity
0.0008
Inclination
88.9721°
RAAN
68.1681°
Arg. of periapsis
58.2072°
True anomaly
301.91086°
Mean anomaly
301.9883°
Eccentric anomaly
301.94958°
Mean motion
3.50817 °/min
Orbital period
102.62 mins
BSTAR
0.00035493
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-13 10:36:48.270Z | 46.906° ENE | 2026-03-13 10:39:48.270Z | 81.62° E | 15.656° | 2026-03-13 10:42:48.270Z | 114.176° SE |
| 9 mins | 2026-03-13 12:18:48.270Z | 349.969° N | 2026-03-13 12:22:48.270Z | 263.651° W | 41.764° | 2026-03-13 12:27:48.270Z | 195.605° SSW |
| 10 mins | 2026-03-13 23:48:48.270Z | 164.29° S | 2026-03-13 23:53:48.270Z | 60.541° ENE | 41.782° | 2026-03-13 23:58:48.270Z | 5.537° NNE |
| 5 mins | 2026-03-14 01:34:48.270Z | 261.982° W | 2026-03-14 01:36:48.270Z | 285.845° WNW | 15.116° | 2026-03-14 01:39:48.270Z | 318.246° 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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