Showing default

JILIN-01 KUANFU 02B 1, 61189

Orbit data source: Space-Track

JILIN-01 KUANFU 02B 1, 61189 is a payload satellite owned by Changguang WJ (CN) in SSO that was launched on Fri, 20 Sep 2024 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.

Loading next visibility...
Identifier
61189, 2024-169A
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
HARB/CGSTL
Mission
Operational Commercial Imaging
Bus & Motor
JL-1, Unknown motor
Mass
230 kg wet, ~200 kg dry
Launch date (UTC)
2024-09-20 (2 years ago)
Launch vehicle
CHANG ZHENG 2D
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
0.514 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 JILIN-01 KUANFU 02B 1
1 61189U 24169A   26163.80601400  .00004119  00000-0  26555-3 0  9995
2 61189  97.5573 253.3901 0003912  74.2810 285.8849 15.08851236 95167
Epoch: 2026-06-12T19:20Z
TLE epoch observation values (Epoch: 2026-06-12T19:20:39.609Z)
Latitude
-0.00012°
Longitude
62.0949°
Altitude
542.04 km
Speed
7.592 km/s
True Right ascension
16h 53m 33s
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
12:42:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.401 km
Perigee altitude
533.991 km
Semi-major axis
6,914.833 km
Eccentricity
0.00039
Inclination
97.5573°
RAAN
253.3901°
Arg. of periapsis
74.281°
True anomaly
285.84178°
Mean anomaly
285.8849°
Eccentric anomaly
285.86334°
Mean motion
3.7746 °/min
Orbital period
95.37 mins
BSTAR
0.00026555
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
|