QIANFAN-152, 69111
Orbit data source: Space-Track
QIANFAN-152, 69111 is a Chinese payload satellite in LEO that was launched on Sun, 17 May 2026 UTC via a CHANG ZHENG 8 launch vehicle from the Wenchang Satellite Launch Center (WSC). 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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69111 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Operational spacecraft
Bus & Motor
QIANFAN, Unknown motor
Mass
267 kg wet, ~267 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 QIANFAN-152
1 69111U 26108H 26170.52785216 -.02108915 00000-0 -15470+1 0 9992
2 69111 89.0101 21.9564 0015585 111.7124 248.5716 14.00002639 4672Epoch: 2026-06-19T12:40Z
TLE epoch observation values (Epoch: 2026-06-19T12:40:06.426Z)
Latitude
-0.00001°
Longitude
-75.82592°
Altitude
900.967 km
Speed
7.399 km/s
True Right ascension
01h 27m 49s
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
08:32:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
902.095 km
Perigee altitude
879.437 km
Semi-major axis
7,268.903 km
Eccentricity
0.00156
Inclination
89.0101°
RAAN
21.9564°
Arg. of periapsis
111.7124°
True anomaly
248.40547°
Mean anomaly
248.5716°
Eccentric anomaly
248.48852°
Mean motion
3.50219 °/min
Orbital period
102.79 mins
BSTAR
-1.547
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Other satellites on launch #108 in the year 2026 (2026-05-17 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-152 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-06-21 01:22:20.759Z | 29.447° NE | 2026-06-21 01:26:20.759Z | 79.508° E | 24.698° | 2026-06-21 01:31:20.759Z | 139.099° SSE |
| 8 mins | 2026-06-21 03:06:20.759Z | 335.054° NNW | 2026-06-21 03:10:20.759Z | 267.282° W | 31.601° | 2026-06-21 03:14:20.759Z | 216.384° SW |
| 5 mins | 2026-06-21 13:01:20.759Z | 93.584° ESE | 2026-06-21 13:03:20.759Z | 70.434° E | 15.273° | 2026-06-21 13:06:20.759Z | 39.077° NE |
| 10 mins | 2026-06-21 14:41:20.759Z | 189.529° SSW | 2026-06-21 14:46:20.759Z | 301.938° NW | 42.319° | 2026-06-21 14:51:20.759Z | 353.488° N |
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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