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
Last TLE update
6 hours ago
Origin
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 (1 year ago)
Launch vehicle
CHANG ZHENG 2C
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 2 m
Radar Cross Section
0.833 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 6 hours ago
0 GEESAT 2-10
1 58914U 24023K   25184.26549344  .00002210  00000-0  23131-3 0  9993
2 58914  49.9930 176.4078 0003315 212.3542 147.7198 14.93388372 77039
Epoch: 2025-07-03T06:22Z
TLE epoch observation values (Epoch: 2025-07-03T06:22:18.633Z)
Latitude
0.00004°
Longitude
159.29547°
Altitude
589.878 km
Speed
7.565 km/s
True Right ascension
11h 45m 37s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-38.12949°
Longitude
19.08196°
Altitude
597.273 km
Speed
7.562 km/s
Apparent Right ascension
06h 32m 45s
Apparent Declination
-68° 38' 32"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
00:00:26
Azimuth
152.116° SSE
Elevation
-39.557°
Doppler factor
1
Orbital elements
Apogee altitude
590.452 km
Perigee altitude
585.833 km
Semi-major axis
6,966.279 km
Eccentricity
0.00033
Inclination
49.993°
RAAN
176.4078°
Arg. of periapsis
212.3542°
True anomaly
Unknown
Mean anomaly
147.7198°
Eccentric anomaly
Unknown
Mean motion
3.73286 °/min
Orbital period
96.44 mins
BSTAR
0.00023131
Loading maneuver chart data...
Loading SW <> Apogee altitude chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

GEESAT 2-10 Visibility forecast

Observer location: undefined°, undefined°

Span
Click to sort rows by Start time (UTC) header in descending order
Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
8 mins2025-07-04 01:47:49.088Z206.827° SW2025-07-04 01:51:49.088Z139.136° SSE32.745°2025-07-04 01:55:49.088Z68.797° E
6 mins2025-07-04 03:29:49.088Z271.35° WNW2025-07-04 03:32:49.088Z345.283° N33.83°2025-07-04 03:35:49.088Z42.285° NE
5 mins2025-07-04 05:11:49.088Z315.359° NNW2025-07-04 05:13:49.088Z349.509° N20.339°2025-07-04 05:16:49.088Z40.195° NE
5 mins2025-07-04 06:53:49.088Z334.305° NNW2025-07-04 06:55:49.088Z16.102° NNE24.951°2025-07-04 06:58:49.088Z69.676° E
7 mins2025-07-04 08:33:49.088Z304.39° NW2025-07-04 08:36:49.088Z308.247° NW44.881°2025-07-04 08:40:49.088Z125.282° SE
|