JILIN-01-04, 43022
Orbit data source: Space-Track
JILIN-01-04, 43022 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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43022 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: 6 hours ago
TLE from 6 hours ago
0 JILIN-01-04
1 43022U 17074A 25261.00340287 .00010175 00000-0 31363-3 0 9993
2 43022 97.4796 0.2639 0006152 96.9187 263.2755 15.33786796432429Epoch: 2025-09-18T00:04Z
TLE epoch observation values (Epoch: 2025-09-18T00:04:54.007Z)
Latitude
-0.00009°
Longitude
1.86764°
Altitude
468.129 km
Speed
7.632 km/s
True Right ascension
00h 01m 03s
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
22:53:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.685 km
Perigee altitude
457.269 km
Semi-major axis
6,839.614 km
Eccentricity
0.00062
Inclination
97.4796°
RAAN
0.2639°
Arg. of periapsis
96.9187°
True anomaly
263.20549°
Mean anomaly
263.2755°
Eccentric anomaly
263.2405°
Mean motion
3.83704 °/min
Orbital period
93.82 mins
BSTAR
0.00031363
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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-01-04 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 | 2025-09-18 06:28:32.029Z | 148.951° SSE | 2025-09-18 06:31:32.029Z | 63.007° ENE | 37.593° | 2025-09-18 06:34:32.029Z | 359.232° N |
| 5 mins | 2025-09-18 19:26:32.029Z | 22.456° NNE | 2025-09-18 19:28:32.029Z | 78.323° E | 41.799° | 2025-09-18 19:31:32.029Z | 182.32° SSW |
| 4 mins | 2025-09-19 05:59:32.029Z | 103.069° ESE | 2025-09-19 06:00:32.029Z | 81.666° E | 18.651° | 2025-09-19 06:03:32.029Z | 21.398° NNE |
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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