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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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: 8 hours ago
TLE from 8 hours ago
0 JILIN-01-08
1 43160U 18008F 26168.15837978 .00004492 00000-0 14003-3 0 9992
2 43160 97.1798 187.4042 0008014 80.2816 279.9332 15.33711922464947Epoch: 2026-06-17T03:48Z
TLE epoch observation values (Epoch: 2026-06-17T03:48:04.012Z)
Latitude
0.00001°
Longitude
-135.0326°
Altitude
466.923 km
Speed
7.633 km/s
True Right ascension
12h 29m 37s
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
22:23:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
467.169 km
Perigee altitude
456.206 km
Semi-major axis
6,839.824 km
Eccentricity
0.0008
Inclination
97.1798°
RAAN
187.4042°
Arg. of periapsis
80.2816°
True anomaly
279.84273°
Mean anomaly
279.9332°
Eccentric anomaly
279.88797°
Mean motion
3.83686 °/min
Orbital period
93.83 mins
BSTAR
0.00014003
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-17 13:45:54.141Z | 33.496° NE | 2026-06-17 13:47:54.141Z | 76.828° E | 30.817° | 2026-06-17 13:50:54.141Z | 163.784° S |
| 4 mins | 2026-06-18 01:51:54.141Z | 212.565° SW | 2026-06-18 01:53:54.141Z | 274.356° WNW | 27.984° | 2026-06-18 01:55:54.141Z | 320.887° NNW |
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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