JILIN-01-08, 43160
Orbit data source: Space-Track
JILIN-01-08, 43160 is a payload satellite owned by Changguang WJ (CN) in SSO that was launched on Fri, 19 Jan 2018 UTC via a CHANG ZHENG 11 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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43160 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changguang WJ
Mission
Operational Commercial Imaging
Bus & Motor
JL-1, Unknown motor
Mass
95 kg wet, 95 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
2.000 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 JILIN-01-08
1 43160U 18008F 25286.59945854 .00008009 00000-0 28448-3 0 9999
2 43160 97.2023 308.1455 0005133 223.2435 136.8403 15.29268119427202Epoch: 2025-10-13T14:23Z
TLE epoch observation values (Epoch: 2025-10-13T14:23:13.217Z)
Latitude
-0.00008°
Longitude
69.94052°
Altitude
483.676 km
Speed
7.622 km/s
True Right ascension
20h 32m 34s
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
20:15:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
478.461 km
Perigee altitude
471.426 km
Semi-major axis
6,853.081 km
Eccentricity
0.00051
Inclination
97.2023°
RAAN
308.1455°
Arg. of periapsis
223.2435°
True anomaly
136.88052°
Mean anomaly
136.8403°
Eccentric anomaly
136.86041°
Mean motion
3.82573 °/min
Orbital period
94.1 mins
BSTAR
0.00028448
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Other satellites on launch #8 in the year 2018 (2018-01-19 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-01-08 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 | 2025-10-14 14:30:16.429Z | 7.187° NNE | 2025-10-14 14:33:16.429Z | 245.217° WSW | 43.53° | 2025-10-14 14:36:16.429Z | 198.248° SSW |
| 4 mins | 2025-10-15 01:05:16.429Z | 121.51° SE | 2025-10-15 01:07:16.429Z | 64.903° ENE | 27.549° | 2025-10-15 01:09:16.429Z | 17.877° NNE |
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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