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: 16 hours ago
TLE from 16 hours ago
0 QIANFAN-15
1 60393U 24140Q 26113.65746876 .00000044 00000-0 48700-4 0 9995
2 60393 88.9679 285.5856 0012959 165.3669 194.7860 13.51008536 85078Epoch: 2026-04-23T15:46Z
TLE epoch observation values (Epoch: 2026-04-23T15:46:45.300Z)
Latitude
-0.00003°
Longitude
-162.80455°
Altitude
1,080.837 km
Speed
7.307 km/s
True Right ascension
19h 02m 20s
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
14:40:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.248 km
Perigee altitude
1,055.955 km
Semi-major axis
7,443.738 km
Eccentricity
0.0013
Inclination
88.9679°
RAAN
285.5856°
Arg. of periapsis
165.3669°
True anomaly
194.74816°
Mean anomaly
194.786°
Eccentric anomaly
194.76707°
Mean motion
3.37953 °/min
Orbital period
106.52 mins
BSTAR
0.0000487
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-04-24 11:25:44.059Z | 161.282° S | 2026-04-24 11:31:44.059Z | 87.854° E | 40.954° | 2026-04-24 11:37:44.059Z | 7.766° NNE |
| 7 mins | 2026-04-24 13:15:44.059Z | 247.873° W | 2026-04-24 13:18:44.059Z | 281.068° WNW | 20.011° | 2026-04-24 13:22:44.059Z | 323.04° NNW |
| 9 mins | 2026-04-24 22:36:44.059Z | 30.546° NE | 2026-04-24 22:40:44.059Z | 76.221° E | 25.52° | 2026-04-24 22:45:44.059Z | 134.171° SE |
| 11 mins | 2026-04-25 00:22:44.059Z | 343.439° N | 2026-04-25 00:27:44.059Z | 278.15° WNW | 34.853° | 2026-04-25 00:33:44.059Z | 209.532° SW |
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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