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: 12 hours ago
TLE from 12 hours ago
0 JILIN-01-08
1 43160U 18008F 25309.95534444 .00007965 00000-0 27881-3 0 9994
2 43160 97.1983 330.7642 0007675 139.7589 220.4221 15.29735055430771Epoch: 2025-11-05T22:55Z
TLE epoch observation values (Epoch: 2025-11-05T22:55:41.759Z)
Latitude
-0.00007°
Longitude
-58.58038°
Altitude
483.721 km
Speed
7.621 km/s
True Right ascension
22h 03m 03s
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
06:33:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
478.806 km
Perigee altitude
468.289 km
Semi-major axis
6,851.685 km
Eccentricity
0.00077
Inclination
97.1983°
RAAN
330.7642°
Arg. of periapsis
139.7589°
True anomaly
220.36511°
Mean anomaly
220.4221°
Eccentric anomaly
220.3936°
Mean motion
3.8269 °/min
Orbital period
94.07 mins
BSTAR
0.00027881
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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 | 2025-11-06 13:38:25.148Z | 54.871° ENE | 2025-11-06 13:40:25.148Z | 98.105° ESE | 19.45° | 2025-11-06 13:42:25.148Z | 138.685° SSE |
| 5 mins | 2025-11-07 01:45:25.148Z | 182.592° SSW | 2025-11-07 01:47:25.148Z | 259.021° W | 42.128° | 2025-11-07 01:50:25.148Z | 340.788° 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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