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, 1.0 m
Radar Cross Section
2.000 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 JILIN-01 KUANFU 01
1 45016U 20003A 26306.81969900 .00002321 00000-0 14128-3 0 9997
2 45016 97.4900 18.0214 0009675 176.3979 183.7323 15.11362387376260Epoch: 2026-11-02T19:40Z
TLE epoch observation values (Epoch: 2026-11-02T19:40:21.993Z)
Latitude
0.00001°
Longitude
40.83852°
Altitude
541.793 km
Speed
7.588 km/s
True Right ascension
01h 12m 05s
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
04:16:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
535.708 km
Perigee altitude
522.342 km
Semi-major axis
6,907.162 km
Eccentricity
0.00097
Inclination
97.49°
RAAN
18.0214°
Arg. of periapsis
176.3979°
True anomaly
183.72509°
Mean anomaly
183.7323°
Eccentric anomaly
183.7287°
Mean motion
3.78089 °/min
Orbital period
95.22 mins
BSTAR
0.00014128
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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 | 2026-11-03 16:54:59.136Z | 54.193° ENE | 2026-11-03 16:56:59.136Z | 90.682° ESE | 19.63° | 2026-11-03 16:58:59.136Z | 129.841° SE |
| 4 mins | 2026-11-03 18:29:59.136Z | 325.892° NNW | 2026-11-03 18:31:59.136Z | 276.392° WNW | 25.436° | 2026-11-03 18:33:59.136Z | 239.159° WSW |
| 6 mins | 2026-11-04 05:09:59.136Z | 182.089° SSW | 2026-11-04 05:12:59.136Z | 260.428° W | 59.119° | 2026-11-04 05:15:59.136Z | 337.24° 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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