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: 7 hours ago
TLE from 7 hours ago
0 JILIN-01-07
1 43159U 18008E 26034.59099927 .00010113 00000-0 32644-3 0 9992
2 43159 97.1894 58.2170 0008983 165.9591 194.1903 15.32278065444524Epoch: 2026-02-03T14:11Z
TLE epoch observation values (Epoch: 2026-02-03T14:11:02.336Z)
Latitude
-0.00003°
Longitude
71.68753°
Altitude
478.095 km
Speed
7.623 km/s
True Right ascension
03h 52m 52s
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
22:52:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
472.106 km
Perigee altitude
459.81 km
Semi-major axis
6,844.095 km
Eccentricity
0.0009
Inclination
97.1894°
RAAN
58.217°
Arg. of periapsis
165.9591°
True anomaly
194.16509°
Mean anomaly
194.1903°
Eccentric anomaly
194.17769°
Mean motion
3.83327 °/min
Orbital period
93.91 mins
BSTAR
0.00032644
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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 | 2026-02-04 01:16:44.554Z | 153.286° SSE | 2026-02-04 01:19:44.554Z | 94.621° ESE | 39.027° | 2026-02-04 01:22:44.554Z | 359.845° N |
| 5 mins | 2026-02-04 14:15:44.554Z | 16.083° NNE | 2026-02-04 14:17:44.554Z | 40.432° NE | 42.565° | 2026-02-04 14:20:44.554Z | 187.405° SSW |
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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