Showing default

JILIN-01 GAOFEN 3I, 46461

Orbit data source: Space-Track

JILIN-01 GAOFEN 3I, 46461 is a payload satellite owned by Changguang WJ (CN) in SSO that was launched on Tue, 15 Sep 2020 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.

Loading next visibility...
Identifier
46461, 2020-065H
Orbit
SSO
Last TLE update
20 hours ago
Origin
Flag of CNCGSTL (CN / PRC)
Manufacturer
Changguang WJ
Mission
Operational Commercial Imaging
Bus & Motor
JL-1, Unknown motor
Mass
42 kg wet, 42 kg dry
Launch date (UTC)
2020-09-15 (5 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

TLE from 20 hours ago
0 JILIN-01 GAOFEN 3I
1 46461U 20065H   25235.98733307  .00024088  00000-0  50423-3 0  9990
2 46461  97.2801 284.7514 0020312 100.0849 260.2693 15.45219796273864
Epoch: 2025-08-23T23:41Z
TLE epoch observation values (Epoch: 2025-08-23T23:41:45.577Z)
Latitude
-0.00001°
Longitude
-43.20272°
Altitude
436.226 km
Speed
7.649 km/s
True Right ascension
18h 59m 00s
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
10:59:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.483 km
Perigee altitude
413.835 km
Semi-major axis
6,805.796 km
Eccentricity
0.00203
Inclination
97.2801°
RAAN
284.7514°
Arg. of periapsis
100.0849°
True anomaly
260.03999°
Mean anomaly
260.2693°
Eccentric anomaly
260.15463°
Mean motion
3.86567 °/min
Orbital period
93.13 mins
BSTAR
0.00050423
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
|