JILIN-01 KUANFU 02B 4, 61192
Orbit data source: Space-Track
JILIN-01 KUANFU 02B 4, 61192 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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61192 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: 5 hours ago
TLE from 5 hours ago
0 JILIN-01 KUANFU 02B 4
1 61192U 24169D 26163.82918242 .00003313 00000-0 21430-3 0 9998
2 61192 97.5531 252.7770 0011718 281.0549 78.9361 15.08830368 95176Epoch: 2026-06-12T19:54Z
TLE epoch observation values (Epoch: 2026-06-12T19:54:01.361Z)
Latitude
-0.00006°
Longitude
53.11832°
Altitude
541.297 km
Speed
7.593 km/s
True Right ascension
16h 51m 06s
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
11:30:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
544.863 km
Perigee altitude
528.657 km
Semi-major axis
6,914.897 km
Eccentricity
0.00117
Inclination
97.5531°
RAAN
252.777°
Arg. of periapsis
281.0549°
True anomaly
79.06792°
Mean anomaly
78.9361°
Eccentric anomaly
79.00201°
Mean motion
3.77454 °/min
Orbital period
95.38 mins
BSTAR
0.0002143
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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 4 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-13 05:35:04.682Z | 141.59° SSE | 2026-06-13 05:38:04.682Z | 69.019° E | 34.96° | 2026-06-13 05:41:04.682Z | 4.352° NNE |
| 5 mins | 2026-06-13 18:46:04.682Z | 17.596° NNE | 2026-06-13 18:48:04.682Z | 91.202° ESE | 44.535° | 2026-06-13 18:51:04.682Z | 188.425° 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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