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: 6 hours ago
TLE from 6 hours ago
0 JILIN-01-08
1 43160U 18008F 26065.28563666 .00009352 00000-0 30365-3 0 9991
2 43160 97.1899 87.4441 0008241 85.7675 274.4508 15.32118134449185Epoch: 2026-03-06T06:51Z
TLE epoch observation values (Epoch: 2026-03-06T06:51:19.007Z)
Latitude
-0.00011°
Longitude
-179.40891°
Altitude
472.173 km
Speed
7.63 km/s
True Right ascension
05h 49m 46s
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
17:17:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
472.075 km
Perigee altitude
460.794 km
Semi-major axis
6,844.571 km
Eccentricity
0.00082
Inclination
97.1899°
RAAN
87.4441°
Arg. of periapsis
85.7675°
True anomaly
274.35664°
Mean anomaly
274.4508°
Eccentric anomaly
274.40372°
Mean motion
3.83287 °/min
Orbital period
93.92 mins
BSTAR
0.00030365
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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 | 2026-03-06 13:42:03.487Z | 44.289° NE | 2026-03-06 13:44:03.487Z | 91.54° ESE | 25.529° | 2026-03-06 13:47:03.487Z | 156.924° SSE |
| 5 mins | 2026-03-07 01:48:03.487Z | 195.574° SSW | 2026-03-07 01:50:03.487Z | 253.217° W | 34.858° | 2026-03-07 01:53:03.487Z | 332.5° 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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