JILIN-01 KUANFU 02B 3, 61191
Orbit data source: Space-Track
JILIN-01 KUANFU 02B 3, 61191 is a payload satellite owned by Changguang WJ (CN) in SSO that was launched on Fri, 20 Sep 2024 UTC via a CHANG ZHENG 2D 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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61191 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
HARB/CGSTL
Mission
Operational Commercial Imaging
Bus & Motor
JL-1, Unknown motor
Mass
230 kg wet, ~200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
0.514 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 JILIN-01 KUANFU 02B 3
1 61191U 24169C 26163.79462858 .00004238 00000-0 27265-3 0 9999
2 61191 97.5566 253.2005 0012638 327.9807 32.0652 15.08861366 95164Epoch: 2026-06-12T19:04Z
TLE epoch observation values (Epoch: 2026-06-12T19:04:15.909Z)
Latitude
-0.00007°
Longitude
66.01527°
Altitude
535.341 km
Speed
7.599 km/s
True Right ascension
16h 52m 48s
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
12:42:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
545.404 km
Perigee altitude
527.926 km
Semi-major axis
6,914.802 km
Eccentricity
0.00126
Inclination
97.5566°
RAAN
253.2005°
Arg. of periapsis
327.9807°
True anomaly
32.14219°
Mean anomaly
32.0652°
Eccentric anomaly
32.10368°
Mean motion
3.77462 °/min
Orbital period
95.37 mins
BSTAR
0.00027265
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Other satellites on launch #169 in the year 2024 (2024-09-20 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.JILIN-01 KUANFU 02B 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-13 06:21:12.114Z | 196.399° SSW | 2026-06-13 06:23:12.114Z | 260.838° W | 37.056° | 2026-06-13 06:26:12.114Z | 332.92° NNW |
| 4 mins | 2026-06-13 17:57:12.114Z | 66.197° ENE | 2026-06-13 17:58:12.114Z | 84.656° E | 17.456° | 2026-06-13 18:01:12.114Z | 136.924° SSE |
| 5 mins | 2026-06-13 19:31:12.114Z | 335.199° NNW | 2026-06-13 19:33:12.114Z | 288.862° WNW | 26.091° | 2026-06-13 19:36:12.114Z | 231.48° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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