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: 9 hours ago
TLE from 9 hours ago
0 JILIN-01 KUANFU 01
1 45016U 20003A 26126.95137414 .00003386 00000-0 20919-3 0 9996
2 45016 97.5034 201.7165 0011362 86.2125 274.0404 15.10492852349100Epoch: 2026-05-06T22:49Z
TLE epoch observation values (Epoch: 2026-05-06T22:49:58.725Z)
Latitude
-0°
Longitude
-5.58269°
Altitude
537.226 km
Speed
7.594 km/s
True Right ascension
13h 26m 51s
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
15:30:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.53 km
Perigee altitude
523.828 km
Semi-major axis
6,909.816 km
Eccentricity
0.00114
Inclination
97.5034°
RAAN
201.7165°
Arg. of periapsis
86.2125°
True anomaly
273.91051°
Mean anomaly
274.0404°
Eccentric anomaly
273.97546°
Mean motion
3.77871 °/min
Orbital period
95.27 mins
BSTAR
0.00020919
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-07 16:54:29.277Z | 56.186° ENE | 2026-05-07 16:56:29.277Z | 90.819° ESE | 16.668° | 2026-05-07 16:58:29.277Z | 127.291° SE |
| 4 mins | 2026-05-07 18:29:29.277Z | 329.758° NNW | 2026-05-07 18:31:29.277Z | 276.693° WNW | 25.689° | 2026-05-07 18:33:29.277Z | 236.365° WSW |
| 6 mins | 2026-05-08 05:10:29.277Z | 179.905° S | 2026-05-08 05:12:29.277Z | 214.25° SW | 40.32° | 2026-05-08 05:16:29.277Z | 341.532° N |
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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