QIANFAN-162, 69121
Orbit data source: Space-Track
QIANFAN-162, 69121 is a Chinese payload satellite in LEO that was launched on Sun, 17 May 2026 UTC via a CHANG ZHENG 8 launch vehicle from the Wenchang Satellite Launch Center (WSC). 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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69121 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 shape, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 QIANFAN-162
1 69121U 26108T 26171.38154698 .00000119 00000-0 64046-4 0 9992
2 69121 89.0109 21.8444 0016738 100.8952 259.4115 14.05908691 4803Epoch: 2026-06-20T09:09Z
TLE epoch observation values (Epoch: 2026-06-20T09:09:25.659Z)
Latitude
0.00004°
Longitude
-24.10949°
Altitude
878.689 km
Speed
7.412 km/s
True Right ascension
01h 27m 22s
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
07:12:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
882.51 km
Perigee altitude
858.245 km
Semi-major axis
7,248.514 km
Eccentricity
0.00167
Inclination
89.0109°
RAAN
21.8444°
Arg. of periapsis
100.8952°
True anomaly
259.22304°
Mean anomaly
259.4115°
Eccentric anomaly
259.31726°
Mean motion
3.51698 °/min
Orbital period
102.36 mins
BSTAR
0.000064046
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Other satellites on launch #108 in the year 2026 (2026-05-17 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-162 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-21 01:07:48.898Z | 38.319° NE | 2026-06-21 01:10:48.898Z | 73.057° E | 18.232° | 2026-06-21 01:14:48.898Z | 121.282° SE |
| 9 mins | 2026-06-21 02:49:48.898Z | 346.411° N | 2026-06-21 02:53:48.898Z | 282.213° WNW | 38.128° | 2026-06-21 02:58:48.898Z | 203.241° SW |
| 9 mins | 2026-06-21 14:18:48.898Z | 170.272° S | 2026-06-21 14:22:48.898Z | 117.688° SE | 43.969° | 2026-06-21 14:27:48.898Z | 3.007° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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