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: 1 day ago
TLE from 1 day ago
0 JILIN-01-08
1 43160U 18008F 26006.28705586 .00007949 00000-0 26805-3 0 9999
2 43160 97.1934 30.1955 0004709 304.3253 55.7543 15.30969368440155Epoch: 2026-01-06T06:53Z
TLE epoch observation values (Epoch: 2026-01-06T06:53:21.626Z)
Latitude
0.00003°
Longitude
-179.01664°
Altitude
474.215 km
Speed
7.63 km/s
True Right ascension
02h 00m 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
06:46:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.086 km
Perigee altitude
466.636 km
Semi-major axis
6,847.998 km
Eccentricity
0.00047
Inclination
97.1934°
RAAN
30.1955°
Arg. of periapsis
304.3253°
True anomaly
55.79892°
Mean anomaly
55.7543°
Eccentric anomaly
55.77661°
Mean motion
3.82999 °/min
Orbital period
94 mins
BSTAR
0.00026805
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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 | 2026-01-07 14:49:46.892Z | 341.876° N | 2026-01-07 14:51:46.892Z | 290.005° WNW | 28.814° | 2026-01-07 14:54:46.892Z | 223.58° SW |
| 5 mins | 2026-01-08 01:22:46.892Z | 156.433° SSE | 2026-01-08 01:24:46.892Z | 118.227° SE | 41.38° | 2026-01-08 01:27:46.892Z | 355.615° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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