QIANFAN-133, 69078
Orbit data source: Space-Track
QIANFAN-133, 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
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-133
1 69078U 26104F 26140.62143142 -.02073720 00000-0 -11119+1 0 9995
2 69078 88.9863 344.7767 0010085 194.9209 165.1684 14.17255778 1177Epoch: 2026-05-20T14:54Z
TLE epoch observation values (Epoch: 2026-05-20T14:54:51.674Z)
Latitude
0.00002°
Longitude
-117.21696°
Altitude
844.731 km
Speed
7.427 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
08:20:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
838.875 km
Perigee altitude
824.333 km
Semi-major axis
7,209.741 km
Eccentricity
0.00101
Inclination
88.9863°
RAAN
344.7767°
Arg. of periapsis
194.9209°
True anomaly
165.19795°
Mean anomaly
165.1684°
Eccentric anomaly
165.18318°
Mean motion
3.54539 °/min
Orbital period
101.54 mins
BSTAR
-1.1119
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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-133 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 01:39:45.363Z | 7.642° NNE | 2026-05-21 01:44:45.363Z | 79.768° E | 42.043° | 2026-05-21 01:49:45.363Z | 169.932° S |
| 4 mins | 2026-05-21 03:24:45.363Z | 301.309° NW | 2026-05-21 03:25:45.363Z | 289.029° WNW | 14.706° | 2026-05-21 03:28:45.363Z | 254.436° W |
| 7 mins | 2026-05-21 13:06:45.363Z | 127.086° SE | 2026-05-21 13:09:45.363Z | 85.156° E | 25.457° | 2026-05-21 13:13:45.363Z | 28.318° NE |
| 8 mins | 2026-05-21 14:48:45.363Z | 224.565° SW | 2026-05-21 14:51:45.363Z | 274.852° WNW | 29.622° | 2026-05-21 14:56:45.363Z | 340.367° 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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