QIANFAN-129, 69074
Orbit data source: Space-Track
QIANFAN-129, 69074 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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69074 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-129
1 69074U 26104B 26140.55130374 -.01981423 00000-0 -10700+1 0 9998
2 69074 88.9866 344.7848 0008650 202.1179 157.9637 14.16689105 1169Epoch: 2026-05-20T13:13Z
TLE epoch observation values (Epoch: 2026-05-20T13:13:52.643Z)
Latitude
-0.00002°
Longitude
-91.89378°
Altitude
845.407 km
Speed
7.427 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
08:19:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
839.766 km
Perigee altitude
827.29 km
Semi-major axis
7,211.665 km
Eccentricity
0.00087
Inclination
88.9866°
RAAN
344.7848°
Arg. of periapsis
202.1179°
True anomaly
158.00085°
Mean anomaly
157.9637°
Eccentric anomaly
157.98228°
Mean motion
3.54397 °/min
Orbital period
101.58 mins
BSTAR
-1.07
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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-129 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 01:40:40.080Z | 6.81° NNE | 2026-05-21 01:45:40.080Z | 66.429° ENE | 42.081° | 2026-05-21 01:50:40.080Z | 170.337° S |
| 4 mins | 2026-05-21 03:25:40.080Z | 304.016° NW | 2026-05-21 03:26:40.080Z | 292.107° WNW | 14.333° | 2026-05-21 03:29:40.080Z | 257.227° W |
| 7 mins | 2026-05-21 13:08:40.080Z | 123.606° SE | 2026-05-21 13:11:40.080Z | 76.329° E | 26.174° | 2026-05-21 13:15:40.080Z | 24.521° NE |
| 8 mins | 2026-05-21 14:49:40.080Z | 220.521° SW | 2026-05-21 14:53:40.080Z | 284.006° WNW | 28.8° | 2026-05-21 14:57:40.080Z | 336.501° NNW |
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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