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: 11 hours ago
TLE from 11 hours ago
0 JILIN-01-08
1 43160U 18008F 25339.31937337 .00009656 00000-0 33097-3 0 9990
2 43160 97.1952 359.2107 0008080 57.4295 302.7726 15.30358040435260Epoch: 2025-12-05T07:39Z
TLE epoch observation values (Epoch: 2025-12-05T07:39:53.859Z)
Latitude
0.00004°
Longitude
169.87311°
Altitude
474.859 km
Speed
7.63 km/s
True Right ascension
23h 56m 50s
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
16:52:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.221 km
Perigee altitude
466.152 km
Semi-major axis
6,849.823 km
Eccentricity
0.00081
Inclination
97.1952°
RAAN
359.2107°
Arg. of periapsis
57.4295°
True anomaly
302.69471°
Mean anomaly
302.7726°
Eccentric anomaly
302.73366°
Mean motion
3.82846 °/min
Orbital period
94.03 mins
BSTAR
0.00033097
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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 | 2025-12-06 01:04:09.504Z | 131.655° SE | 2025-12-06 01:06:09.504Z | 85.725° E | 28.677° | 2025-12-06 01:09:09.504Z | 11.023° NNE |
| 5 mins | 2025-12-06 14:03:09.504Z | 30.06° NE | 2025-12-06 14:05:09.504Z | 79.023° E | 35.658° | 2025-12-06 14:08:09.504Z | 170.979° S |
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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