QIANFAN-15, 60393
Orbit data source: Space-Track
QIANFAN-15, 60393 is a Chinese payload satellite in LEO that was launched on Tue, 06 Aug 2024 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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60393 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Operational Commercial Communications
Bus & Motor
QIANFAN, Unknown motor
Mass
267 kg wet, ~267 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 5.0 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-15
1 60393U 24140Q 26054.11077013 .00000093 00000-0 12601-3 0 9994
2 60393 88.9731 291.7856 0012444 353.8700 6.2297 13.50997311 77030Epoch: 2026-02-23T02:39Z
TLE epoch observation values (Epoch: 2026-02-23T02:39:30.539Z)
Latitude
0.00001°
Longitude
98.899°
Altitude
1,062.331 km
Speed
7.325 km/s
True Right ascension
19h 27m 08s
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
12:54:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.906 km
Perigee altitude
1,056.38 km
Semi-major axis
7,443.78 km
Eccentricity
0.00124
Inclination
88.9731°
RAAN
291.7856°
Arg. of periapsis
353.87°
True anomaly
6.2452°
Mean anomaly
6.2297°
Eccentric anomaly
6.23745°
Mean motion
3.3795 °/min
Orbital period
106.52 mins
BSTAR
0.00012601
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Other satellites on launch #140 in the year 2024 (2024-08-06 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-15 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 | 2026-02-23 15:12:56.116Z | 137.006° SSE | 2026-02-23 15:17:56.116Z | 83.543° E | 28.175° | 2026-02-23 15:22:56.116Z | 23.403° NE |
| 10 mins | 2026-02-23 16:59:56.116Z | 214.984° SW | 2026-02-23 17:04:56.116Z | 283.304° WNW | 32.076° | 2026-02-23 17:09:56.116Z | 340.546° N |
| 5 mins | 2026-02-24 02:24:56.116Z | 56.789° ENE | 2026-02-24 02:26:56.116Z | 76.873° E | 14.803° | 2026-02-24 02:29:56.116Z | 105.233° ESE |
| 11 mins | 2026-02-24 04:08:56.116Z | 358.019° N | 2026-02-24 04:13:56.116Z | 291.144° WNW | 44.637° | 2026-02-24 04:19:56.116Z | 187.282° SSW |
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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