Showing default

CENTISPACE-1 S10, 62579

Orbit data source: Space-Track

CENTISPACE-1 S10, 62579 is a payload satellite owned by Centispace (CN) in LEO that was launched on Mon, 13 Jan 2025 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
62579, 2025-007E
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
DFH Shenzhen
Mission
Operational Commercial Nav/Com
Bus & Motor
WK01, Unknown motor
Mass
140 kg wet, 140 kg dry
Launch date (UTC)
2025-01-13 (10 months ago)
Launch vehicle
JIELONG-3
Launch site
Yellow Sea Launch Area, China (YSLA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.9 m
Radar Cross Section
0.833 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 CENTISPACE-1 S10
1 62579U 25007E   25324.53962165  .00000029  00000-0  72586-4 0  9999
2 62579  54.9866 317.8180 0027963 154.3434 205.8939 14.29805247 45634
Epoch: 2025-11-20T12:57Z
TLE epoch observation values (Epoch: 2025-11-20T12:57:03.310Z)
Latitude
-0.00003°
Longitude
63.75864°
Altitude
811.476 km
Speed
7.439 km/s
True Right ascension
21h 11m 16s
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
11:15:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
812.399 km
Perigee altitude
772.297 km
Semi-major axis
7,170.485 km
Eccentricity
0.0028
Inclination
54.9866°
RAAN
317.818°
Arg. of periapsis
154.3434°
True anomaly
205.7544°
Mean anomaly
205.8939°
Eccentric anomaly
205.82411°
Mean motion
3.57454 °/min
Orbital period
100.71 mins
BSTAR
0.000072586
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
|