QIANFAN-144, 69089
Orbit data source: Space-Track
QIANFAN-144, 69089 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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69089 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-144
1 69089U 26104S 26140.12055928 -.02028840 00000-0 -96088+0 0 9996
2 69089 88.9864 344.8320 0005821 94.4598 265.7259 14.23790117 1109Epoch: 2026-05-20T02:53Z
TLE epoch observation values (Epoch: 2026-05-20T02:53:36.321Z)
Latitude
-0.00007°
Longitude
63.64599°
Altitude
815.936 km
Speed
7.445 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
09:06:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
813.693 km
Perigee altitude
805.325 km
Semi-major axis
7,187.646 km
Eccentricity
0.00058
Inclination
88.9864°
RAAN
344.832°
Arg. of periapsis
94.4598°
True anomaly
265.65939°
Mean anomaly
265.7259°
Eccentric anomaly
265.69264°
Mean motion
3.56175 °/min
Orbital period
101.07 mins
BSTAR
-0.96088
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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-144 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 01:25:35.977Z | 14.313° NNE | 2026-05-21 01:30:35.977Z | 91.774° ESE | 36.06° | 2026-05-21 01:35:35.977Z | 160.278° S |
| 5 mins | 2026-05-21 03:09:35.977Z | 309.779° NW | 2026-05-21 03:11:35.977Z | 281.389° WNW | 19.21° | 2026-05-21 03:14:35.977Z | 243.462° WSW |
| 5 mins | 2026-05-21 12:51:35.977Z | 104.646° ESE | 2026-05-21 12:53:35.977Z | 77.329° E | 18.817° | 2026-05-21 12:56:35.977Z | 38.964° NE |
| 9 mins | 2026-05-21 14:30:35.977Z | 202.631° SW | 2026-05-21 14:34:35.977Z | 266.164° W | 36.744° | 2026-05-21 14:39:35.977Z | 346.032° 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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