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: 19 hours ago
TLE from 19 hours ago
0 JILIN-01-07
1 43159U 18008E 25256.29954918 .00005476 00000-0 19589-3 0 9993
2 43159 97.2037 279.2826 0008189 342.2865 17.8089 15.29160978422609Epoch: 2025-09-13T07:11Z
TLE epoch observation values (Epoch: 2025-09-13T07:11:21.049Z)
Latitude
0°
Longitude
178.91°
Altitude
476.081 km
Speed
7.631 km/s
True Right ascension
18h 37m 07s
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
480.876 km
Perigee altitude
469.652 km
Semi-major axis
6,853.401 km
Eccentricity
0.00082
Inclination
97.2037°
RAAN
279.2826°
Arg. of periapsis
342.2865°
True anomaly
17.83763°
Mean anomaly
17.8089°
Eccentric anomaly
17.82326°
Mean motion
3.82546 °/min
Orbital period
94.11 mins
BSTAR
0.00019589
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-14 13:36:29.512Z | 54.306° ENE | 2025-09-14 13:38:29.512Z | 90.916° ESE | 16.623° | 2025-09-14 13:40:29.512Z | 129.623° SE |
| 4 mins | 2025-09-14 15:10:29.512Z | 325.276° NNW | 2025-09-14 15:11:29.512Z | 301.67° NW | 22.536° | 2025-09-14 15:14:29.512Z | 236.193° WSW |
| 5 mins | 2025-09-15 01:44:29.512Z | 173.314° S | 2025-09-15 01:46:29.512Z | 331.438° NNW | 42.053° | 2025-09-15 01:49:29.512Z | 346.54° 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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