JILIN-01-07, 43159
Orbit data source: Space-Track
JILIN-01-07, 43159 is a Chinese payload satellite 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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43159 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-01-07
1 43159U 18008E 25302.48319770 .00010760 00000-0 37008-3 0 9995
2 43159 97.1987 324.0252 0009794 154.1948 205.9783 15.30203067429662Epoch: 2025-10-29T11:35Z
TLE epoch observation values (Epoch: 2025-10-29T11:35:48.281Z)
Latitude
-0.00008°
Longitude
112.01835°
Altitude
484.353 km
Speed
7.62 km/s
True Right ascension
21h 36m 06s
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
18:57:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
478.859 km
Perigee altitude
465.44 km
Semi-major axis
6,850.286 km
Eccentricity
0.00098
Inclination
97.1987°
RAAN
324.0252°
Arg. of periapsis
154.1948°
True anomaly
205.92919°
Mean anomaly
205.9783°
Eccentric anomaly
205.95374°
Mean motion
3.82807 °/min
Orbital period
94.04 mins
BSTAR
0.00037008
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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-01-07 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-30 01:50:56.956Z | 183.129° SSW | 2025-10-30 01:53:56.956Z | 281.34° WNW | 39.274° | 2025-10-30 01:56:56.956Z | 339.075° N |
| 6 mins | 2025-10-30 14:49:56.956Z | 353.529° N | 2025-10-30 14:52:56.956Z | 279.91° WNW | 32.256° | 2025-10-30 14:55:56.956Z | 216.948° SW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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