QIANFAN-19, 61552
Orbit data source: Space-Track
QIANFAN-19, 61552 is a Chinese payload satellite in LEO that was launched on Tue, 15 Oct 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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61552 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GESIH/SECM
Mission
Partially 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: 11 hours ago
TLE from 11 hours ago
0 QIANFAN-19
1 61552U 24185A 25308.87363411 .00000652 00000-0 33430-3 0 9999
2 61552 88.9797 82.2735 0008889 73.4912 286.7251 14.14232831 64319Epoch: 2025-11-04T20:58Z
TLE epoch observation values (Epoch: 2025-11-04T20:58:01.987Z)
Latitude
0.00002°
Longitude
83.41082°
Altitude
846.125 km
Speed
7.431 km/s
True Right ascension
05h 29m 05s
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
04:13:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
848.301 km
Perigee altitude
835.465 km
Semi-major axis
7,220.02 km
Eccentricity
0.00089
Inclination
88.9797°
RAAN
82.2735°
Arg. of periapsis
73.4912°
True anomaly
286.62752°
Mean anomaly
286.7251°
Eccentric anomaly
286.67631°
Mean motion
3.53782 °/min
Orbital period
101.76 mins
BSTAR
0.0003343
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Other satellites on launch #185 in the year 2024 (2024-10-15 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-19 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-05 08:58:11.782Z | 152.569° SSE | 2025-11-05 09:02:11.782Z | 97.39° ESE | 35.857° | 2025-11-05 09:07:11.782Z | 13.469° NNE |
| 6 mins | 2025-11-05 10:42:11.782Z | 246.787° WSW | 2025-11-05 10:44:11.782Z | 273.055° WNW | 19.166° | 2025-11-05 10:48:11.782Z | 323.552° NNW |
| 9 mins | 2025-11-05 21:20:11.782Z | 1.288° NNE | 2025-11-05 21:24:11.782Z | 177.654° S | 44.841° | 2025-11-05 21:29:11.782Z | 182.321° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
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