Showing default

GEESAT 2-10, 58914

Orbit data source: Space-Track

GEESAT 2-10, 58914 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Fri, 02 Feb 2024 UTC via a CHANG ZHENG 2C 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
58914, 2024-023K
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Taizhou Xingkong
Mission
Operational Commercial Navigation
Bus & Motor
GEESAT1, Unknown motor
Mass
130 kg wet, 130 kg dry
Launch date (UTC)
2024-02-02 (2 years ago)
Launch vehicle
CHANG ZHENG 2C
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.833 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 GEESAT 2-10
1 58914U 24023K   25249.28625362  .00004785  00000-0  52163-3 0  9998
2 58914  49.9922 231.6924 0007912  61.9522 298.2218 14.89464384 86732
Epoch: 2025-09-06T06:52Z
TLE epoch observation values (Epoch: 2025-09-06T06:52:12.312Z)
Latitude
-0.00003°
Longitude
143.01881°
Altitude
597.545 km
Speed
7.564 km/s
True Right ascension
15h 26m 46s
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
18:04:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.891 km
Perigee altitude
594.848 km
Semi-major axis
6,978.507 km
Eccentricity
0.00079
Inclination
49.9922°
RAAN
231.6924°
Arg. of periapsis
61.9522°
True anomaly
298.14188°
Mean anomaly
298.2218°
Eccentric anomaly
298.18184°
Mean motion
3.72305 °/min
Orbital period
96.69 mins
BSTAR
0.00052163
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
|