QIANFAN-156, 69115
Orbit data source: Space-Track
QIANFAN-156, 69115 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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69115 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-156
1 69115U 26108M 26170.85474434 .00000048 00000-0 21426-4 0 9995
2 69115 89.0113 21.9133 0018835 96.9786 263.3538 14.04087717 4727Epoch: 2026-06-19T20:30Z
TLE epoch observation values (Epoch: 2026-06-19T20:30:49.910Z)
Latitude
-0.00008°
Longitude
166.1276°
Altitude
884.313 km
Speed
7.409 km/s
True Right ascension
01h 27m 39s
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
07:12:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
890.313 km
Perigee altitude
862.984 km
Semi-major axis
7,254.785 km
Eccentricity
0.00188
Inclination
89.0113°
RAAN
21.9133°
Arg. of periapsis
96.9786°
True anomaly
263.13948°
Mean anomaly
263.3538°
Eccentric anomaly
263.24663°
Mean motion
3.51242 °/min
Orbital period
102.49 mins
BSTAR
0.000021426
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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-156 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 02:10:25.448Z | 6.593° NNE | 2026-06-21 02:15:25.448Z | 108.657° ESE | 43.328° | 2026-06-21 02:20:25.448Z | 173.828° S |
| 4 mins | 2026-06-21 03:55:25.448Z | 305.137° NW | 2026-06-21 03:57:25.448Z | 281.96° WNW | 13.817° | 2026-06-21 03:59:25.448Z | 260.111° W |
| 8 mins | 2026-06-21 13:41:25.448Z | 138.099° SSE | 2026-06-21 13:45:25.448Z | 78.705° E | 29.88° | 2026-06-21 13:49:25.448Z | 22.248° NNE |
| 8 mins | 2026-06-21 15:24:25.448Z | 228.207° WSW | 2026-06-21 15:27:25.448Z | 269.15° W | 25.428° | 2026-06-21 15:32:25.448Z | 334.822° 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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