JILIN-01 KUANFU 01, 45016
Orbit data source: Space-Track
JILIN-01 KUANFU 01, 45016 is a payload satellite owned by Changguang WJ (CN) in SSO that was launched on Wed, 15 Jan 2020 UTC via a CHANG ZHENG 2D 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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45016 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
1,250 kg wet, 1,250 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 hours ago
TLE from 3 hours ago
0 JILIN-01 KUANFU 01
1 45016U 20003A 26050.15926503 .00003685 00000-0 23100-3 0 9996
2 45016 97.5134 126.4327 0009586 356.4399 3.6760 15.09918056337514Epoch: 2026-02-19T03:49Z
TLE epoch observation values (Epoch: 2026-02-19T03:49:20.498Z)
Latitude
-0.00008°
Longitude
-80.01726°
Altitude
532.908 km
Speed
7.6 km/s
True Right ascension
08h 25m 43s
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
09:51:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.059 km
Perigee altitude
526.809 km
Semi-major axis
6,911.571 km
Eccentricity
0.00096
Inclination
97.5134°
RAAN
126.4327°
Arg. of periapsis
356.4399°
True anomaly
3.68305°
Mean anomaly
3.676°
Eccentric anomaly
3.67952°
Mean motion
3.77727 °/min
Orbital period
95.31 mins
BSTAR
0.000231
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Other satellites on launch #3 in the year 2020 (2020-01-15 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 KUANFU 01 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 | 2026-02-19 17:07:56.121Z | 50.99° ENE | 2026-02-19 17:09:56.121Z | 90.923° ESE | 22.313° | 2026-02-19 17:12:56.121Z | 147.656° SSE |
| 4 mins | 2026-02-19 18:42:56.121Z | 323.064° NNW | 2026-02-19 18:44:56.121Z | 279.594° WNW | 20.331° | 2026-02-19 18:46:56.121Z | 244.908° WSW |
| 5 mins | 2026-02-20 05:24:56.121Z | 203.526° SW | 2026-02-20 05:26:56.121Z | 275.922° WNW | 34.914° | 2026-02-20 05:29:56.121Z | 333.108° 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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