QIANFAN-132, 69077
Orbit data source: Space-Track
QIANFAN-132, 69077 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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69077 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-132
1 69077U 26104E 26140.61209770 -.01947571 00000-0 -94987+0 0 9999
2 69077 88.9863 344.7753 0004562 146.8279 213.3199 14.22075796 1170Epoch: 2026-05-20T14:41Z
TLE epoch observation values (Epoch: 2026-05-20T14:41:25.241Z)
Latitude
-0.00001°
Longitude
-113.84903°
Altitude
824.142 km
Speed
7.44 km/s
True Right ascension
22h 59m 06s
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
08:20:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
818.571 km
Perigee altitude
812.008 km
Semi-major axis
7,193.426 km
Eccentricity
0.00046
Inclination
88.9863°
RAAN
344.7753°
Arg. of periapsis
146.8279°
True anomaly
213.2912°
Mean anomaly
213.3199°
Eccentric anomaly
213.30555°
Mean motion
3.55746 °/min
Orbital period
101.2 mins
BSTAR
-0.94987
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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-132 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 01:24:59.703Z | 18.032° NNE | 2026-05-21 01:28:59.703Z | 81.328° E | 35.426° | 2026-05-21 01:33:59.703Z | 158.235° S |
| 6 mins | 2026-05-21 03:07:59.703Z | 313.498° NW | 2026-05-21 03:09:59.703Z | 285.671° WNW | 19.627° | 2026-05-21 03:13:59.703Z | 236.805° WSW |
| 5 mins | 2026-05-21 12:49:59.703Z | 105.173° ESE | 2026-05-21 12:51:59.703Z | 78.676° E | 18.317° | 2026-05-21 12:54:59.703Z | 40.333° NE |
| 9 mins | 2026-05-21 14:28:59.703Z | 201.136° SSW | 2026-05-21 14:32:59.703Z | 263.406° W | 37.383° | 2026-05-21 14:37:59.703Z | 346.441° 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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