QIANFAN-170, 69387
Orbit data source: Space-Track
QIANFAN-170, 69387 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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69387 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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-170
1 69387U 26124F 26171.41666498 .00000076 00000-0 29480-4 0 9999
2 69387 88.9983 1.6696 0003280 121.5307 238.6203 14.19183817 2278Epoch: 2026-06-20T09:59Z
TLE epoch observation values (Epoch: 2026-06-20T09:59:59.854Z)
Latitude
-0.00004°
Longitude
-56.96139°
Altitude
832.398 km
Speed
7.436 km/s
True Right ascension
00h 06m 40s
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
07:13:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
827.429 km
Perigee altitude
822.704 km
Semi-major axis
7,203.204 km
Eccentricity
0.00033
Inclination
88.9983°
RAAN
1.6696°
Arg. of periapsis
121.5307°
True anomaly
238.58822°
Mean anomaly
238.6203°
Eccentric anomaly
238.60426°
Mean motion
3.55021 °/min
Orbital period
101.4 mins
BSTAR
0.00002948
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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-170 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-21 00:07:25.172Z | 27.18° NE | 2026-06-21 00:11:25.172Z | 80.003° E | 25.275° | 2026-06-21 00:15:25.172Z | 136.346° SSE |
| 8 mins | 2026-06-21 01:49:25.172Z | 334.274° NNW | 2026-06-21 01:53:25.172Z | 269.687° W | 28.562° | 2026-06-21 01:57:25.172Z | 218.723° SW |
| 9 mins | 2026-06-21 13:11:25.172Z | 181.677° SSW | 2026-06-21 13:15:25.172Z | 219.571° SW | 44.367° | 2026-06-21 13:20:25.172Z | 356.762° 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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