Showing default

GEESAT 3-08, 61018

Orbit data source: Space-Track

GEESAT 3-08, 61018 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Thu, 05 Sep 2024 UTC via a CHANG ZHENG 6 launch vehicle from the Taiyaun Space Center, China (TSC). 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
61018, 2024-159H
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)
2024-09-05 (2 years ago)
Launch vehicle
CHANG ZHENG 6
Launch site
Taiyaun Space Center, China (TSC)
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: 10 hours ago

TLE from 10 hours ago
0 GEESAT 3-08
1 61018U 24159H   26171.41679741  .00001626  00000-0  21852-3 0  9999
2 61018  50.0062  68.1119 0027628 105.2496 255.1499 14.84226390 97256
Epoch: 2026-06-20T10:00Z
TLE epoch observation values (Epoch: 2026-06-20T10:00:11.296Z)
Latitude
-0.00008°
Longitude
9.43304°
Altitude
621.562 km
Speed
7.547 km/s
True Right ascension
04h 32m 26s
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
07:16:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
636.098 km
Perigee altitude
597.447 km
Semi-major axis
6,994.91 km
Eccentricity
0.00276
Inclination
50.0062°
RAAN
68.1119°
Arg. of periapsis
105.2496°
True anomaly
254.84415°
Mean anomaly
255.1499°
Eccentric anomaly
254.997°
Mean motion
3.70997 °/min
Orbital period
97.04 mins
BSTAR
0.00021852
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
|