QIANFAN-155, 69114
Orbit data source: Space-Track
QIANFAN-155, 69114 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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69114 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: 11 hours ago
TLE from 11 hours ago
0 QIANFAN-155
1 69114U 26108L 26171.38226047 .00000082 00000-0 45728-4 0 9997
2 69114 89.0111 21.8632 0017638 97.7967 262.5215 14.01011633 4798Epoch: 2026-06-20T09:10Z
TLE epoch observation values (Epoch: 2026-06-20T09:10:27.304Z)
Latitude
-0.0001°
Longitude
-24.34825°
Altitude
895.011 km
Speed
7.404 km/s
True Right ascension
01h 27m 27s
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
07:15:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
900.087 km
Perigee altitude
874.458 km
Semi-major axis
7,265.41 km
Eccentricity
0.00176
Inclination
89.0111°
RAAN
21.8632°
Arg. of periapsis
97.7967°
True anomaly
262.32116°
Mean anomaly
262.5215°
Eccentric anomaly
262.42132°
Mean motion
3.50472 °/min
Orbital period
102.72 mins
BSTAR
0.000045728
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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-155 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 | 2026-06-21 01:12:00.412Z | 35.578° NE | 2026-06-21 01:16:00.412Z | 84.875° E | 20.145° | 2026-06-21 01:19:00.412Z | 121.554° SE |
| 9 mins | 2026-06-21 02:55:00.412Z | 341.567° N | 2026-06-21 02:59:00.412Z | 266.207° W | 36.18° | 2026-06-21 03:04:00.412Z | 205.005° SW |
| 9 mins | 2026-06-21 14:26:00.412Z | 176.413° S | 2026-06-21 14:30:00.412Z | 159.787° S | 44.82° | 2026-06-21 14:35:00.412Z | 359.612° 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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