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GALILEO 30 (10E), 59600

Orbit data source: Space-Track

GALILEO 30 (10E), 59600 is a payload satellite owned by EU SPA (ESA) that was launched on Sun, 28 Apr 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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.

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Identifier
59600, 2024-079C
Orbit
Active
Country
Flag of ESAESA
Related business
Manufacturer
OHB
Mission
Operational Civil Navigation
Bus & Motor
GALILEO, AOCS
Mass
733 kg wet, 660 kg dry
Launch date (UTC)
2024-04-28 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 7.3 m
Radar Cross Section
9.223 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 GALILEO 30 (10E)
1 59600U 24079C   26170.34920996 -.00000013  00000-0  00000-0 0  9995
2 59600  55.1161 101.0181 0002202  52.0058 307.9926  1.70473950 13409
Epoch: 2026-06-19T08:22Z
TLE epoch observation values (Epoch: 2026-06-19T08:22:51.740Z)
Latitude
0.00008°
Longitude
67.7223°
Altitude
23,218.431 km
Speed
3.67 km/s
True Right ascension
06h 44m 04s
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
21:38:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
23,228.711 km
Perigee altitude
23,215.675 km
Semi-major axis
29,600.33 km
Eccentricity
0.00022
Inclination
55.1161°
RAAN
101.0181°
Arg. of periapsis
52.0058°
True anomaly
307.97271°
Mean anomaly
307.9926°
Eccentric anomaly
307.98266°
Mean motion
0.42619 °/min
Orbital period
844.7 mins
BSTAR
0
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Other satellites on launch #79 in the year 2024 (2024-04-28 UTC)

Documentation

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