QIANFAN-122, 68649
Orbit data source: Space-Track
QIANFAN-122, 68649 is a Chinese payload satellite in LEO that was launched on Tue, 07 Apr 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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68649 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: 15 hours ago
TLE from 15 hours ago
0 QIANFAN-122
1 68649U 26075P 26171.23327729 .00000081 00000-0 10751-3 0 9991
2 68649 88.9894 320.6776 0001692 100.9226 259.2116 13.51013292 10217Epoch: 2026-06-20T05:35Z
TLE epoch observation values (Epoch: 2026-06-20T05:35:55.157Z)
Latitude
-0°
Longitude
-31.75306°
Altitude
1,071.722 km
Speed
7.316 km/s
True Right ascension
21h 22m 42s
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
07:14:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,066.843 km
Perigee altitude
1,064.324 km
Semi-major axis
7,443.721 km
Eccentricity
0.00017
Inclination
88.9894°
RAAN
320.6776°
Arg. of periapsis
100.9226°
True anomaly
259.19255°
Mean anomaly
259.2116°
Eccentric anomaly
259.20208°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.00010751
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Other satellites on launch #75 in the year 2026 (2026-04-07 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-122 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-06-20 22:12:17.564Z | 3.821° NNE | 2026-06-20 22:17:17.564Z | 101.573° ESE | 44.735° | 2026-06-20 22:23:17.564Z | 178.906° S |
| 5 mins | 2026-06-21 00:01:17.564Z | 304.416° NW | 2026-06-21 00:03:17.564Z | 284.11° WNW | 14.627° | 2026-06-21 00:06:17.564Z | 256.555° W |
| 11 mins | 2026-06-21 10:09:17.564Z | 166.561° S | 2026-06-21 10:14:17.564Z | 75.535° E | 43.598° | 2026-06-21 10:20:17.564Z | 3.792° NNE |
| 7 mins | 2026-06-21 11:58:17.564Z | 253.012° W | 2026-06-21 12:01:17.564Z | 283.398° WNW | 16.638° | 2026-06-21 12:05:17.564Z | 321.917° NNW |
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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