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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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, 1.0 m
Radar Cross Section
2.000 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 JILIN-01-07
1 43159U 18008E 26276.98709573 .00006067 00000-0 17379-3 0 9999
2 43159 97.1752 294.1193 0009032 38.1884 321.9998 15.36239582481693Epoch: 2026-10-03T23:41Z
TLE epoch observation values (Epoch: 2026-10-03T23:41:25.071Z)
Latitude
-0.00008°
Longitude
-73.92197°
Altitude
455.496 km
Speed
7.642 km/s
True Right ascension
19h 36m 28s
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
04:55:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.346 km
Perigee altitude
448.005 km
Semi-major axis
6,832.312 km
Eccentricity
0.0009
Inclination
97.1752°
RAAN
294.1193°
Arg. of periapsis
38.1884°
True anomaly
321.93602°
Mean anomaly
321.9998°
Eccentric anomaly
321.96792°
Mean motion
3.84319 °/min
Orbital period
93.67 mins
BSTAR
0.00017379
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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 | 2026-10-04 14:19:03.331Z | 2.041° NNE | 2026-10-04 14:22:03.331Z | 259.729° W | 57.969° | 2026-10-04 14:25:03.331Z | 204.165° SW |
| 4 mins | 2026-10-05 00:51:03.331Z | 126.335° SE | 2026-10-05 00:53:03.331Z | 68.622° E | 32.994° | 2026-10-05 00:55:03.331Z | 17° NNE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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