JILIN-01-06, 43024
Orbit data source: Space-Track
JILIN-01-06, 43024 is a payload satellite owned by Changguang WJ (CN) in SSO that was launched on Tue, 21 Nov 2017 UTC via a CHANG ZHENG 6 launch vehicle from the Taiyaun Space Center, China (TSC). 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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43024 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
HARB/CIOMP
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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 JILIN-01-06
1 43024U 17074C 26268.79547301 .00006047 00000-0 18214-3 0 9998
2 43024 97.4840 13.2895 0005554 233.8335 126.2395 15.34711002489262Epoch: 2026-09-25T19:05Z
TLE epoch observation values (Epoch: 2026-09-25T19:05:28.868Z)
Latitude
0.00005°
Longitude
82.30645°
Altitude
467.135 km
Speed
7.631 km/s
True Right ascension
00h 53m 09s
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
18:49:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
462.526 km
Perigee altitude
454.931 km
Semi-major axis
6,836.866 km
Eccentricity
0.00056
Inclination
97.484°
RAAN
13.2895°
Arg. of periapsis
233.8335°
True anomaly
126.29081°
Mean anomaly
126.2395°
Eccentric anomaly
126.26516°
Mean motion
3.83935 °/min
Orbital period
93.77 mins
BSTAR
0.00018214
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Other satellites on launch #74 in the year 2017 (2017-11-21 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-01-06 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 | 2026-09-26 07:45:44.666Z | 233.785° WSW | 2026-09-26 07:46:44.666Z | 262.806° W | 26.768° | 2026-09-26 07:49:44.666Z | 322.815° NNW |
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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