Showing default

GEESAT 1-03, 52787

Orbit data source: Space-Track

GEESAT 1-03, 52787 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Thu, 02 Jun 2022 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
52787, 2022-058C
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
GWCG
Mission
Operational Commercial Navigation
Bus & Motor
GPS100, Unknown motor
Mass
130 kg wet, 130 kg dry
Launch date (UTC)
2022-06-02 (4 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, Large (>1 m²)

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

TLE from 2 days ago
0 GEESAT 1-03
1 52787U 22058C   26171.40397159  .00000905  00000-0  14269-3 0  9990
2 52787  49.9857 186.5338 0007658 118.0547 242.1165 14.81384839220418
Epoch: 2026-06-20T09:41Z
TLE epoch observation values (Epoch: 2026-06-20T09:41:43.145Z)
Latitude
-0.00005°
Longitude
132.48491°
Altitude
628.009 km
Speed
7.544 km/s
True Right ascension
12h 26m 08s
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
21:52:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
631.08 km
Perigee altitude
620.353 km
Semi-major axis
7,003.853 km
Eccentricity
0.00077
Inclination
49.9857°
RAAN
186.5338°
Arg. of periapsis
118.0547°
True anomaly
242.03897°
Mean anomaly
242.1165°
Eccentric anomaly
242.07773°
Mean motion
3.70286 °/min
Orbital period
97.22 mins
BSTAR
0.00014269
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
|