QIANFAN-115, 68642
Orbit data source: Space-Track
QIANFAN-115, 68642 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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68642 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, 1.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-115
1 68642U 26075G 26171.44305139 .00000098 00000-0 13380-3 0 9997
2 68642 88.9894 320.6887 0001928 100.9595 259.1774 13.51018944 10234Epoch: 2026-06-20T10:37Z
TLE epoch observation values (Epoch: 2026-06-20T10:37:59.640Z)
Latitude
0.00009°
Longitude
-107.4674°
Altitude
1,071.735 km
Speed
7.316 km/s
True Right ascension
21h 22m 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
07:14:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,066.998 km
Perigee altitude
1,064.128 km
Semi-major axis
7,443.7 km
Eccentricity
0.00019
Inclination
88.9894°
RAAN
320.6887°
Arg. of periapsis
100.9595°
True anomaly
259.1557°
Mean anomaly
259.1774°
Eccentric anomaly
259.16655°
Mean motion
3.37956 °/min
Orbital period
106.52 mins
BSTAR
0.0001338
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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-115 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-06-20 21:53:06.526Z | 8.708° NNE | 2026-06-20 21:59:06.526Z | 78.212° E | 40.904° | 2026-06-20 22:05:06.526Z | 166.198° S |
| 7 mins | 2026-06-20 23:42:06.526Z | 320.238° NNW | 2026-06-20 23:45:06.526Z | 287.67° WNW | 19.993° | 2026-06-20 23:49:06.526Z | 245.47° WSW |
| 11 mins | 2026-06-21 09:51:06.526Z | 154.223° SSE | 2026-06-21 09:56:06.526Z | 91.377° ESE | 38.399° | 2026-06-21 10:02:06.526Z | 10.591° NNE |
| 9 mins | 2026-06-21 11:39:06.526Z | 235.451° WSW | 2026-06-21 11:43:06.526Z | 279.166° WNW | 22.323° | 2026-06-21 11:48:06.526Z | 331.061° 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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