QIANFAN-139, 69084
Orbit data source: Space-Track
QIANFAN-139, 69084 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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69084 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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-139
1 69084U 26104M 26140.61315949 .00000061 00000-0 19764-4 0 9999
2 69084 88.9870 344.7749 0001985 182.5883 177.5300 14.25562063 1171Epoch: 2026-05-20T14:42Z
TLE epoch observation values (Epoch: 2026-05-20T14:42:56.979Z)
Latitude
-0.00007°
Longitude
-114.23272°
Altitude
811.09 km
Speed
7.447 km/s
True Right ascension
22h 59m 05s
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
08:20:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
804.972 km
Perigee altitude
802.121 km
Semi-major axis
7,181.684 km
Eccentricity
0.0002
Inclination
88.987°
RAAN
344.7749°
Arg. of periapsis
182.5883°
True anomaly
177.53098°
Mean anomaly
177.53°
Eccentric anomaly
177.53049°
Mean motion
3.56618 °/min
Orbital period
100.95 mins
BSTAR
0.000019764
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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-139 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 01:23:40.868Z | 14.336° NNE | 2026-05-21 01:28:40.868Z | 86.332° E | 35.027° | 2026-05-21 01:33:40.868Z | 158.557° S |
| 6 mins | 2026-05-21 03:06:40.868Z | 318.922° NNW | 2026-05-21 03:09:40.868Z | 277.259° WNW | 19.459° | 2026-05-21 03:12:40.868Z | 240.032° WSW |
| 5 mins | 2026-05-21 12:46:40.868Z | 102.172° ESE | 2026-05-21 12:48:40.868Z | 76.141° E | 16.658° | 2026-05-21 12:51:40.868Z | 39.559° NE |
| 8 mins | 2026-05-21 14:25:40.868Z | 201.098° SSW | 2026-05-21 14:29:40.868Z | 292.101° WNW | 38.343° | 2026-05-21 14:33:40.868Z | 347.226° 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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