QIANFAN-3, 60381
Orbit data source: Space-Track
QIANFAN-3, 60381 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.
Focus sentinelFocus sentinel
Request partner network tasking
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
60381 intel report (Beta)
Focus sentinelFocus sentinel
Edit Public Description
Focus sentinelFocus sentinel
Create New Watchlist
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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-3
1 60381U 24140C 26054.23814882 .00000111 00000-0 15358-3 0 9990
2 60381 88.9712 291.7419 0014073 357.8037 2.3050 13.51002409 77106Epoch: 2026-02-23T05:42Z
TLE epoch observation values (Epoch: 2026-02-23T05:42:56.058Z)
Latitude
0.00001°
Longitude
52.87343°
Altitude
1,061.053 km
Speed
7.327 km/s
True Right ascension
19h 26m 58s
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
14:28:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.1 km
Perigee altitude
1,055.148 km
Semi-major axis
7,443.761 km
Eccentricity
0.00141
Inclination
88.9712°
RAAN
291.7419°
Arg. of periapsis
357.8037°
True anomaly
2.3115°
Mean anomaly
2.305°
Eccentric anomaly
2.30825°
Mean motion
3.37952 °/min
Orbital period
106.52 mins
BSTAR
0.00015358
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #140 in the year 2024 (2024-08-06 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.QIANFAN-3 Visibility forecast
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-02-23 14:44:40.721Z | 113.704° SE | 2026-02-23 14:48:40.721Z | 74.379° E | 18.181° | 2026-02-23 14:52:40.721Z | 34.536° NE |
| 11 mins | 2026-02-23 16:29:40.721Z | 191.869° SSW | 2026-02-23 16:34:40.721Z | 275.665° WNW | 42.525° | 2026-02-23 16:40:40.721Z | 352.862° N |
| 12 mins | 2026-02-24 03:38:40.721Z | 10.308° NNE | 2026-02-24 03:44:40.721Z | 108.689° ESE | 40.759° | 2026-02-24 03:50:40.721Z | 168.08° S |
| 8 mins | 2026-02-24 05:26:40.721Z | 322.252° NNW | 2026-02-24 05:29:40.721Z | 290.945° WNW | 19.888° | 2026-02-24 05:34:40.721Z | 240.655° WSW |
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 |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
|---|