Showing default

YAOGAN-43 02D, 60948

Orbit data source: Space-Track

YAOGAN-43 02D, 60948 is a payload satellite owned by PLA GAD (CN) in LEO that was launched on Tue, 03 Sep 2024 UTC via a CHANG ZHENG 4B launch vehicle from the Xichang Space Center, China (XSC). 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
60948, 2024-156D
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SAST
Mission
Operational Defense Communications
Bus & Motor
Unknown
Mass
~300 kg wet, ~300 kg dry
Launch date (UTC)
2024-09-03 (2 years ago)
Launch vehicle
CHANG ZHENG 4B
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 2.5 m
Radar Cross Section
11.063 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 YAOGAN-43 02D
1 60948U 24156D   26075.29785738  .00008372  00000-0  34460-3 0  9994
2 60948  34.9928  62.1634 0004136 154.6323 205.4595 15.23387224 85273
Epoch: 2026-03-16T07:08Z
TLE epoch observation values (Epoch: 2026-03-16T07:08:54.877Z)
Latitude
-0.00004°
Longitude
141.04235°
Altitude
497.105 km
Speed
7.617 km/s
True Right ascension
04h 08m 39s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
02:07:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.729 km
Perigee altitude
496.04 km
Semi-major axis
6,877.021 km
Eccentricity
0.00041
Inclination
34.9928°
RAAN
62.1634°
Arg. of periapsis
154.6323°
True anomaly
205.43914°
Mean anomaly
205.4595°
Eccentric anomaly
205.44932°
Mean motion
3.80577 °/min
Orbital period
94.59 mins
BSTAR
0.0003446
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
|