JILIN-01 KUANFU 02B 5, 61193
Orbit data source: Space-Track
JILIN-01 KUANFU 02B 5, 61193 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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61193 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 5
1 61193U 24169E 26163.81707142 .00003111 00000-0 20120-3 0 9994
2 61193 97.5574 253.5399 0011906 308.4359 51.5801 15.08873678 95179Epoch: 2026-06-12T19:36Z
TLE epoch observation values (Epoch: 2026-06-12T19:36:34.970Z)
Latitude
0.00004°
Longitude
58.25311°
Altitude
537.598 km
Speed
7.597 km/s
True Right ascension
16h 54m 09s
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
12:42:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
544.86 km
Perigee altitude
528.395 km
Semi-major axis
6,914.765 km
Eccentricity
0.00119
Inclination
97.5574°
RAAN
253.5399°
Arg. of periapsis
308.4359°
True anomaly
51.68709°
Mean anomaly
51.5801°
Eccentric anomaly
51.63359°
Mean motion
3.77465 °/min
Orbital period
95.37 mins
BSTAR
0.0002012
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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 5 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-13 05:18:32.832Z | 117.19° SE | 2026-06-13 05:20:32.832Z | 77.952° E | 23.158° | 2026-06-13 05:23:32.832Z | 18.501° NNE |
| 4 mins | 2026-06-13 06:53:32.832Z | 230.033° WSW | 2026-06-13 06:55:32.832Z | 270.447° WNW | 19.499° | 2026-06-13 06:57:32.832Z | 307.023° NW |
| 5 mins | 2026-06-13 18:28:32.832Z | 36.995° NE | 2026-06-13 18:30:32.832Z | 86.919° E | 33.87° | 2026-06-13 18:33:32.832Z | 165.158° S |
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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