QIANFAN-129, 69075
Orbit data source: Space-Track
QIANFAN-129, 69075 is a Chinese payload satellite in LEO that was launched on Tue, 12 May 2026 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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69075 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
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 QIANFAN-129
1 69075U 26104C 26155.27921988 .00000134 00000-0 50726-4 0 9997
2 69075 88.9863 343.0702 0004794 147.0030 213.1464 14.25500113 3263Epoch: 2026-06-04T06:42Z
TLE epoch observation values (Epoch: 2026-06-04T06:42:04.597Z)
Latitude
0.00006°
Longitude
-10.17472°
Altitude
812.758 km
Speed
7.445 km/s
True Right ascension
22h 52m 16s
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
02:48:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
807.198 km
Perigee altitude
800.312 km
Semi-major axis
7,181.892 km
Eccentricity
0.00048
Inclination
88.9863°
RAAN
343.0702°
Arg. of periapsis
147.003°
True anomaly
213.11638°
Mean anomaly
213.1464°
Eccentric anomaly
213.13139°
Mean motion
3.56603 °/min
Orbital period
100.95 mins
BSTAR
0.000050726
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Other satellites on launch #104 in the year 2026 (2026-05-12 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-129 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-06 23:19:15.496Z | 45.242° ENE | 2026-06-06 23:22:15.496Z | 80.496° E | 14.331° | 2026-06-06 23:24:15.496Z | 104.493° ESE |
| 8 mins | 2026-06-07 01:00:15.496Z | 348.259° N | 2026-06-07 01:03:15.496Z | 289.145° WNW | 41.335° | 2026-06-07 01:08:15.496Z | 195.88° SSW |
| 8 mins | 2026-06-07 12:19:15.496Z | 152.448° SSE | 2026-06-07 12:23:15.496Z | 78.592° E | 37.091° | 2026-06-07 12:27:15.496Z | 13.923° NNE |
| 5 mins | 2026-06-07 14:02:15.496Z | 251.3° W | 2026-06-07 14:04:15.496Z | 278.244° WNW | 17.884° | 2026-06-07 14:07:15.496Z | 317.04° 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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