QIANFAN-132, 69078
Orbit data source: Space-Track
QIANFAN-132, 69078 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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69078 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Operational spacecraft
Bus & Motor
QIANFAN, Unknown motor
Mass
267 kg wet, ~267 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 QIANFAN-132
1 69078U 26104F 26155.29548267 .00000118 00000-0 50436-4 0 9997
2 69078 88.9863 343.0915 0004892 136.8174 223.3400 14.18146846 3259Epoch: 2026-06-04T07:05Z
TLE epoch observation values (Epoch: 2026-06-04T07:05:29.702Z)
Latitude
0.00003°
Longitude
-16.02405°
Altitude
837.244 km
Speed
7.433 km/s
True Right ascension
22h 52m 21s
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
03:33:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
832.106 km
Perigee altitude
825.055 km
Semi-major axis
7,206.718 km
Eccentricity
0.00049
Inclination
88.9863°
RAAN
343.0915°
Arg. of periapsis
136.8174°
True anomaly
223.30154°
Mean anomaly
223.34°
Eccentric anomaly
223.32077°
Mean motion
3.54762 °/min
Orbital period
101.48 mins
BSTAR
0.000050436
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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 | 2026-06-07 00:00:57.615Z | 17.549° NNE | 2026-06-07 00:05:57.615Z | 86.069° E | 31.64° | 2026-06-07 00:09:57.615Z | 147.747° SSE |
| 7 mins | 2026-06-07 01:43:57.615Z | 326.589° NNW | 2026-06-07 01:46:57.615Z | 285.967° WNW | 22.858° | 2026-06-07 01:50:57.615Z | 232.484° WSW |
| 4 mins | 2026-06-07 11:27:57.615Z | 95.879° ESE | 2026-06-07 11:29:57.615Z | 70.438° E | 15.641° | 2026-06-07 11:31:57.615Z | 46.488° ENE |
| 8 mins | 2026-06-07 13:06:57.615Z | 196.968° SSW | 2026-06-07 13:10:57.615Z | 291.181° WNW | 40.392° | 2026-06-07 13:14:57.615Z | 348.802° 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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