Showing default

CENTISPACE-2 S4, 68353

Orbit data source: Space-Track

CENTISPACE-2 S4, 68353 is a payload satellite owned by Centispace (CN) in LEO that was launched on Sun, 22 Mar 2026 UTC via a JIELONG-3 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
68353, 2026-060D
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
DFH Shenzhen
Mission
Operational spacecraft
Bus & Motor
WK01, Unknown motor
Mass
140 kg wet, 140 kg dry
Launch date (UTC)
2026-03-22 (3 months ago)
Launch vehicle
JIELONG-3
Launch site
Yellow Sea Launch Area, China (YSLA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.0 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 CENTISPACE-2 S4
1 68353U 26060D   26171.33402934  .00000522  00000-0  13436-3 0  9993
2 68353  54.9841  24.4945 0013483 306.8834  53.0924 14.64252966 13212
Epoch: 2026-06-20T08:01Z
TLE epoch observation values (Epoch: 2026-06-20T08:01:00.134Z)
Latitude
-0.00006°
Longitude
-4.30624°
Altitude
674.831 km
Speed
7.523 km/s
True Right ascension
01h 37m 58s
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
07:21:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
688.957 km
Perigee altitude
669.925 km
Semi-major axis
7,057.578 km
Eccentricity
0.00135
Inclination
54.9841°
RAAN
24.4945°
Arg. of periapsis
306.8834°
True anomaly
53.21607°
Mean anomaly
53.0924°
Eccentric anomaly
53.15422°
Mean motion
3.66066 °/min
Orbital period
98.34 mins
BSTAR
0.00013436
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
|