QIANFAN-137, 69082
Orbit data source: Space-Track
QIANFAN-137, 69082 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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69082 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-137
1 69082U 26104K 26140.12101527 -.01829611 00000-0 -90984+0 0 9999
2 69082 88.9865 344.8322 0001539 230.1427 129.9628 14.20809515 1108Epoch: 2026-05-20T02:54Z
TLE epoch observation values (Epoch: 2026-05-20T02:54:15.719Z)
Latitude
-0.00004°
Longitude
63.48158°
Altitude
826.383 km
Speed
7.439 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
08:18:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
820.674 km
Perigee altitude
818.459 km
Semi-major axis
7,197.704 km
Eccentricity
0.00015
Inclination
88.9865°
RAAN
344.8322°
Arg. of periapsis
230.1427°
True anomaly
129.97632°
Mean anomaly
129.9628°
Eccentric anomaly
129.96956°
Mean motion
3.55428 °/min
Orbital period
101.29 mins
BSTAR
-0.90984
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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-137 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 01:28:32.385Z | 11.609° NNE | 2026-05-21 01:33:32.385Z | 76.814° E | 37.553° | 2026-05-21 01:38:32.385Z | 161.15° S |
| 6 mins | 2026-05-21 03:12:32.385Z | 315.398° NNW | 2026-05-21 03:14:32.385Z | 289.945° WNW | 18.12° | 2026-05-21 03:18:32.385Z | 241.536° WSW |
| 6 mins | 2026-05-21 12:55:32.385Z | 112.736° SE | 2026-05-21 12:58:32.385Z | 70.621° E | 20.504° | 2026-05-21 13:01:32.385Z | 33.764° NE |
| 9 mins | 2026-05-21 14:35:32.385Z | 207.695° SW | 2026-05-21 14:39:32.385Z | 275.221° WNW | 34.877° | 2026-05-21 14:44:32.385Z | 345.089° 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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