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: 8 hours ago
TLE from 8 hours ago
0 JILIN-01-06
1 43024U 17074C 25293.64170637 .00014661 00000-0 51113-3 0 9999
2 43024 97.4786 29.6025 0007677 20.8851 339.2702 15.29713992437166Epoch: 2025-10-20T15:24Z
TLE epoch observation values (Epoch: 2025-10-20T15:24:03.430Z)
Latitude
0.00005°
Longitude
129.24711°
Altitude
474.846 km
Speed
7.631 km/s
True Right ascension
01h 58m 24s
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
18:02:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
478.883 km
Perigee altitude
468.363 km
Semi-major axis
6,851.76 km
Eccentricity
0.00077
Inclination
97.4786°
RAAN
29.6025°
Arg. of periapsis
20.8851°
True anomaly
339.23903°
Mean anomaly
339.2702°
Eccentric anomaly
339.25462°
Mean motion
3.82684 °/min
Orbital period
94.07 mins
BSTAR
0.00051113
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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 | 2025-10-21 05:40:47.906Z | 110.762° ESE | 2025-10-21 05:42:47.906Z | 75.335° E | 16.536° | 2025-10-21 05:44:47.906Z | 34.981° NE |
| 4 mins | 2025-10-21 07:14:47.906Z | 228.22° WSW | 2025-10-21 07:15:47.906Z | 252.532° W | 22.155° | 2025-10-21 07:18:47.906Z | 317.451° NNW |
| 4 mins | 2025-10-21 18:40:47.906Z | 62.709° ENE | 2025-10-21 18:41:47.906Z | 84.974° E | 19.993° | 2025-10-21 18:44:47.906Z | 145.778° SSE |
| 4 mins | 2025-10-21 20:13:47.906Z | 324.15° NNW | 2025-10-21 20:15:47.906Z | 279.737° WNW | 18.582° | 2025-10-21 20:17:47.906Z | 244.15° WSW |
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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