QIANFAN-135, 69081
Orbit data source: Space-Track
QIANFAN-135, 69081 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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69081 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-135
1 69081U 26104J 26155.27110324 .00000117 00000-0 48495-4 0 9999
2 69081 88.9863 343.0879 0004224 158.9872 201.1492 14.19621563 3251Epoch: 2026-06-04T06:30Z
TLE epoch observation values (Epoch: 2026-06-04T06:30:23.319Z)
Latitude
-0.00007°
Longitude
-7.22703°
Altitude
832.524 km
Speed
7.435 km/s
True Right ascension
22h 52m 21s
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
03:42:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
826.627 km
Perigee altitude
820.543 km
Semi-major axis
7,201.722 km
Eccentricity
0.00042
Inclination
88.9863°
RAAN
343.0879°
Arg. of periapsis
158.9872°
True anomaly
201.13174°
Mean anomaly
201.1492°
Eccentric anomaly
201.14047°
Mean motion
3.55131 °/min
Orbital period
101.37 mins
BSTAR
0.000048495
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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-135 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 23:23:54.997Z | 47.145° ENE | 2026-06-06 23:26:54.997Z | 84.552° E | 16.015° | 2026-06-06 23:28:54.997Z | 108.848° ESE |
| 8 mins | 2026-06-07 01:04:54.997Z | 345.579° N | 2026-06-07 01:07:54.997Z | 291.884° WNW | 39.501° | 2026-06-07 01:12:54.997Z | 199.832° SSW |
| 9 mins | 2026-06-07 12:26:54.997Z | 158.431° S | 2026-06-07 12:30:54.997Z | 72.884° E | 40.371° | 2026-06-07 12:35:54.997Z | 7.333° NNE |
| 4 mins | 2026-06-07 14:10:54.997Z | 261.441° W | 2026-06-07 14:12:54.997Z | 287.163° WNW | 15.614° | 2026-06-07 14:14:54.997Z | 311.149° NW |
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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