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: 5 hours ago
TLE from 5 hours ago
0 JILIN-01-08
1 43160U 18008F 26214.60437808 .00006559 00000-0 20034-3 0 9999
2 43160 97.1804 232.5773 0004130 263.0885 96.9889 15.34214797472065Epoch: 2026-08-02T14:30Z
TLE epoch observation values (Epoch: 2026-08-02T14:30:18.266Z)
Latitude
0.00003°
Longitude
63.80174°
Altitude
466.715 km
Speed
7.633 km/s
True Right ascension
15h 30m 18s
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
09:41:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.015 km
Perigee altitude
457.367 km
Semi-major axis
6,838.328 km
Eccentricity
0.00041
Inclination
97.1804°
RAAN
232.5773°
Arg. of periapsis
263.0885°
True anomaly
97.03587°
Mean anomaly
96.9889°
Eccentric anomaly
97.01239°
Mean motion
3.83812 °/min
Orbital period
93.8 mins
BSTAR
0.00020034
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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 | 2026-08-03 01:35:07.693Z | 184.96° SSW | 2026-08-03 01:38:07.693Z | 264.238° W | 37.849° | 2026-08-03 01:41:07.693Z | 336.42° NNW |
| 6 mins | 2026-08-03 14:32:07.693Z | 354.513° N | 2026-08-03 14:35:07.693Z | 290.975° WNW | 31.604° | 2026-08-03 14:38:07.693Z | 219.186° SW |
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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