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: 19 hours ago
TLE from 19 hours ago
0 JILIN-01-08
1 43160U 18008F 25256.29702977 .00004883 00000-0 17808-3 0 9994
2 43160 97.2052 278.8113 0006286 3.0758 357.0519 15.28593064422579Epoch: 2025-09-13T07:07Z
TLE epoch observation values (Epoch: 2025-09-13T07:07:43.372Z)
Latitude
-0.00009°
Longitude
179.34818°
Altitude
478.819 km
Speed
7.629 km/s
True Right ascension
18h 35m 14s
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
19:02:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.272 km
Perigee altitude
472.654 km
Semi-major axis
6,855.1 km
Eccentricity
0.00063
Inclination
97.2052°
RAAN
278.8113°
Arg. of periapsis
3.0758°
True anomaly
357.04819°
Mean anomaly
357.0519°
Eccentric anomaly
357.05005°
Mean motion
3.82404 °/min
Orbital period
94.14 mins
BSTAR
0.00017808
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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 | 2025-09-14 13:33:29.013Z | 54.028° ENE | 2025-09-14 13:35:29.013Z | 89.727° E | 16.137° | 2025-09-14 13:37:29.013Z | 128.164° SE |
| 4 mins | 2025-09-14 15:07:29.013Z | 327.641° NNW | 2025-09-14 15:09:29.013Z | 275.213° WNW | 23.042° | 2025-09-14 15:11:29.013Z | 236.41° WSW |
| 5 mins | 2025-09-15 01:41:29.013Z | 171.003° S | 2025-09-15 01:43:29.013Z | 309.554° NW | 44.632° | 2025-09-15 01:46:29.013Z | 346.785° 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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