Showing default

JILIN-01 GAOFEN 3D 5, 52390

Orbit data source: Space-Track

JILIN-01 GAOFEN 3D 5, 52390 is a payload satellite owned by Changguang WJ (CN) in SSO that was launched on Sat, 30 Apr 2022 UTC via a CHANG ZHENG 11 launch vehicle from the Yellow Sea Launch Area, China (YSLA). 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.

Not visible in the next 10 days
Identifier
52390, 2022-046C
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Changguang WJ
Mission
Operational Commercial Imaging
Bus & Motor
JL-1, Unknown motor
Mass
43 kg wet, 43 kg dry
Launch date (UTC)
2022-04-30 (4 years ago)
Launch vehicle
CHANG ZHENG 11
Launch site
Yellow Sea Launch Area, China (YSLA)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 JILIN-01 GAOFEN 3D 5
1 52390U 22046C   26100.30304069  .00674259  21282-3  12240-2 0  9999
2 52390  97.4795 217.7544 0006938 252.6302 107.4218 16.01477475219948
Epoch: 2026-04-10T07:16Z
TLE epoch observation values (Epoch: 2026-04-10T07:16:22.715Z)
Latitude
-0.00005°
Longitude
-89.87888°
Altitude
274.908 km
Speed
7.742 km/s
True Right ascension
14h 31m 01s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
20:04:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
271.798 km
Perigee altitude
262.577 km
Semi-major axis
6,645.325 km
Eccentricity
0.00069
Inclination
97.4795°
RAAN
217.7544°
Arg. of periapsis
252.6302°
True anomaly
107.49764°
Mean anomaly
107.4218°
Eccentric anomaly
107.45972°
Mean motion
4.00653 °/min
Orbital period
89.85 mins
BSTAR
0.001224
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|