QIANFAN-135, 69080
Orbit data source: Space-Track
QIANFAN-135, 69080 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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69080 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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-135
1 69080U 26104H 26140.54556074 -.02144476 00000-0 -10998+1 0 9992
2 69080 88.9863 344.7837 0004037 144.8631 215.2826 14.19811252 1162Epoch: 2026-05-20T13:05Z
TLE epoch observation values (Epoch: 2026-05-20T13:05:36.447Z)
Latitude
-0.00003°
Longitude
-89.82174°
Altitude
831.419 km
Speed
7.436 km/s
True Right ascension
22h 59m 08s
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
08:18:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
825.85 km
Perigee altitude
820.036 km
Semi-major axis
7,201.08 km
Eccentricity
0.0004
Inclination
88.9863°
RAAN
344.7837°
Arg. of periapsis
144.8631°
True anomaly
215.25589°
Mean anomaly
215.2826°
Eccentric anomaly
215.26924°
Mean motion
3.55179 °/min
Orbital period
101.36 mins
BSTAR
-1.0998
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-05-21 01:31:28.318Z | 12.919° NNE | 2026-05-21 01:36:28.318Z | 103.761° ESE | 38.268° | 2026-05-21 01:40:28.318Z | 161.626° S |
| 5 mins | 2026-05-21 03:15:28.318Z | 307.077° NW | 2026-05-21 03:17:28.318Z | 280.182° WNW | 17.372° | 2026-05-21 03:20:28.318Z | 245.116° WSW |
| 7 mins | 2026-05-21 12:57:28.318Z | 117.132° SE | 2026-05-21 13:00:28.318Z | 75.733° E | 21.483° | 2026-05-21 13:04:28.318Z | 27.876° NE |
| 8 mins | 2026-05-21 14:38:28.318Z | 214.005° SW | 2026-05-21 14:41:28.318Z | 265.239° W | 33.663° | 2026-05-21 14:46:28.318Z | 342.69° 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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