QIANFAN-136, 69081
Orbit data source: Space-Track
QIANFAN-136, 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
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 QIANFAN-136
1 69081U 26104J 26140.12133586 -.01842498 00000-0 -91922+0 0 9999
2 69081 88.9866 344.8320 0002293 162.0517 198.0755 14.20663066 1104Epoch: 2026-05-20T02:54Z
TLE epoch observation values (Epoch: 2026-05-20T02:54:43.418Z)
Latitude
0.00001°
Longitude
63.36565°
Altitude
827.735 km
Speed
7.438 km/s
True Right ascension
22h 59m 19s
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
08:22:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
821.712 km
Perigee altitude
818.411 km
Semi-major axis
7,198.199 km
Eccentricity
0.00023
Inclination
88.9866°
RAAN
344.832°
Arg. of periapsis
162.0517°
True anomaly
198.06735°
Mean anomaly
198.0755°
Eccentric anomaly
198.07142°
Mean motion
3.55392 °/min
Orbital period
101.3 mins
BSTAR
-0.91922
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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-136 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 | 2026-05-21 01:29:19.751Z | 11.957° NNE | 2026-05-21 01:34:19.751Z | 83.763° E | 37.988° | 2026-05-21 01:39:19.751Z | 162.248° S |
| 5 mins | 2026-05-21 03:13:19.751Z | 313.383° NW | 2026-05-21 03:15:19.751Z | 287.457° WNW | 17.991° | 2026-05-21 03:18:19.751Z | 249.205° W |
| 6 mins | 2026-05-21 12:56:19.751Z | 112.071° ESE | 2026-05-21 12:58:19.751Z | 84.989° E | 20.705° | 2026-05-21 13:02:19.751Z | 32.782° NE |
| 9 mins | 2026-05-21 14:36:19.751Z | 208.711° SW | 2026-05-21 14:40:19.751Z | 277.55° WNW | 34.531° | 2026-05-21 14:45:19.751Z | 345.122° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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