QIANFAN-181, 69398
Orbit data source: Space-Track
QIANFAN-181, 69398 is a Chinese payload satellite in LEO that was launched on Thu, 04 Jun 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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69398 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GESIH
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: 13 hours ago
TLE from 13 hours ago
0 QIANFAN-181
1 69398U 26124S 26171.29198971 .00000074 00000-0 29705-4 0 9991
2 69398 88.9983 1.6881 0002648 109.7220 250.4254 14.16649438 2254Epoch: 2026-06-20T07:00Z
TLE epoch observation values (Epoch: 2026-06-20T07:00:27.910Z)
Latitude
-0.00005°
Longitude
-11.9369°
Altitude
840.395 km
Speed
7.432 km/s
True Right ascension
00h 06m 45s
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
07:13:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
835.572 km
Perigee altitude
831.753 km
Semi-major axis
7,211.799 km
Eccentricity
0.00026
Inclination
88.9983°
RAAN
1.6881°
Arg. of periapsis
109.722°
True anomaly
250.39681°
Mean anomaly
250.4254°
Eccentric anomaly
250.41111°
Mean motion
3.54387 °/min
Orbital period
101.58 mins
BSTAR
0.000029705
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Other satellites on launch #124 in the year 2026 (2026-06-04 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-181 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 | 2026-06-21 00:32:20.640Z | 14.298° NNE | 2026-06-21 00:37:20.640Z | 95.551° ESE | 36.649° | 2026-06-21 00:42:20.640Z | 161.382° S |
| 5 mins | 2026-06-21 02:16:20.640Z | 310.711° NW | 2026-06-21 02:18:20.640Z | 283.108° WNW | 18.991° | 2026-06-21 02:21:20.640Z | 245.173° WSW |
| 5 mins | 2026-06-21 11:59:20.640Z | 104.727° ESE | 2026-06-21 12:01:20.640Z | 76.454° E | 19.75° | 2026-06-21 12:04:20.640Z | 37.739° NE |
| 9 mins | 2026-06-21 13:38:20.640Z | 204.347° SW | 2026-06-21 13:42:20.640Z | 266° W | 35.737° | 2026-06-21 13:47:20.640Z | 344.913° 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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