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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Edit Public Description
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, 0.8 m
Radar Cross Section
2.000 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 JILIN-01-06
1 43024U 17074C 25259.61567834 .00010022 00000-0 36092-3 0 9993
2 43024 97.4773 355.4030 0008756 127.4869 232.7168 15.28740043431961Epoch: 2025-09-16T14:46Z
TLE epoch observation values (Epoch: 2025-09-16T14:46:34.608Z)
Latitude
-0.00004°
Longitude
137.95537°
Altitude
486.319 km
Speed
7.62 km/s
True Right ascension
23h 41m 36s
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
03:03:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.537 km
Perigee altitude
470.533 km
Semi-major axis
6,854.672 km
Eccentricity
0.00088
Inclination
97.4773°
RAAN
355.403°
Arg. of periapsis
127.4869°
True anomaly
232.63702°
Mean anomaly
232.7168°
Eccentric anomaly
232.6769°
Mean motion
3.8244 °/min
Orbital period
94.13 mins
BSTAR
0.00036092
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-17 19:36:22.709Z | 1.159° NNE | 2025-09-17 19:39:22.709Z | 293.636° NW | 38.632° | 2025-09-17 19:42:22.709Z | 209.807° SW |
| 5 mins | 2025-09-18 06:11:22.709Z | 141.398° SSE | 2025-09-18 06:13:22.709Z | 93.653° ESE | 34.762° | 2025-09-18 06:16:22.709Z | 4.693° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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