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, 1.0 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 26276.94319617 .00004219 00000-0 12698-3 0 9999
2 43160 97.1794 293.2535 0007495 55.0243 305.1704 15.34867374481625Epoch: 2026-10-03T22:38Z
TLE epoch observation values (Epoch: 2026-10-03T22:38:12.149Z)
Latitude
0.00005°
Longitude
-58.94067°
Altitude
461.481 km
Speed
7.638 km/s
True Right ascension
19h 33m 00s
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
03:31:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.375 km
Perigee altitude
453.127 km
Semi-major axis
6,836.388 km
Eccentricity
0.00075
Inclination
97.1794°
RAAN
293.2535°
Arg. of periapsis
55.0243°
True anomaly
305.10015°
Mean anomaly
305.1704°
Eccentric anomaly
305.13528°
Mean motion
3.83975 °/min
Orbital period
93.76 mins
BSTAR
0.00012698
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-10-04 13:17:53.815Z | 54.255° ENE | 2026-10-04 13:19:53.815Z | 95.809° ESE | 19.644° | 2026-10-04 13:21:53.815Z | 136.485° SSE |
| 5 mins | 2026-10-05 01:22:53.815Z | 178.172° S | 2026-10-05 01:24:53.815Z | 310.368° NW | 65.471° | 2026-10-05 01:27:53.815Z | 344.613° N |
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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