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: 10 hours ago
TLE from 10 hours ago
0 JILIN-01-04
1 43022U 17074A 25302.54051392 .00015114 00000-0 44311-3 0 9999
2 43022 97.4804 42.3676 0003545 310.6218 49.4716 15.35282787438791Epoch: 2025-10-29T12:58Z
TLE epoch observation values (Epoch: 2025-10-29T12:58:20.402Z)
Latitude
-0.00009°
Longitude
169.67042°
Altitude
461.614 km
Speed
7.637 km/s
True Right ascension
02h 49m 28s
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
19:00:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.452 km
Perigee altitude
454.606 km
Semi-major axis
6,835.166 km
Eccentricity
0.00035
Inclination
97.4804°
RAAN
42.3676°
Arg. of periapsis
310.6218°
True anomaly
49.50249°
Mean anomaly
49.4716°
Eccentric anomaly
49.48704°
Mean motion
3.84078 °/min
Orbital period
93.73 mins
BSTAR
0.00044311
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-30 06:19:00.626Z | 132.635° SE | 2025-10-30 06:22:00.626Z | 57.423° ENE | 27.083° | 2025-10-30 06:24:00.626Z | 14.371° NNE |
| 5 mins | 2025-10-30 19:16:00.626Z | 37.462° NE | 2025-10-30 19:18:00.626Z | 91.096° ESE | 31.61° | 2025-10-30 19:21:00.626Z | 166.225° S |
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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