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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Edit Public Description
Identifier
Orbit
Country
ESARelated business
Manufacturer
OHB
Mission
Operational Civil Navigation
Bus & Motor
GALILEO, AOCS
Mass
733 kg wet, 660 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 7.3 m
Radar Cross Section
9.223 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 GALILEO 30 (10E)
1 59600U 24079C 25273.14749599 .00000046 00000-0 00000-0 0 9999
2 59600 54.9485 108.3523 0003863 101.3985 258.7203 1.70474422 8934Epoch: 2025-09-30T03:32Z
TLE epoch observation values (Epoch: 2025-09-30T03:32:23.653Z)
Latitude
0.00004°
Longitude
46.11504°
Altitude
23,224.645 km
Speed
3.669 km/s
True Right ascension
07h 13m 25s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
12:44:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
23,233.579 km
Perigee altitude
23,210.71 km
Semi-major axis
29,600.282 km
Eccentricity
0.00039
Inclination
54.9485°
RAAN
108.3523°
Arg. of periapsis
101.3985°
True anomaly
258.67689°
Mean anomaly
258.7203°
Eccentric anomaly
258.6986°
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)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GALILEO 30 (10E) Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 410 mins | 2025-09-30 19:05:26.286Z | 277.374° WNW | 2025-09-30 22:28:26.286Z | 58.587° ENE | 44.791° | 2025-10-01 01:55:26.286Z | 165.754° S |
| 28 mins | 2025-10-01 09:48:26.286Z | 53.929° ENE | 2025-10-01 10:02:26.286Z | 49.334° ENE | 10.314° | 2025-10-01 10:16:26.286Z | 44.836° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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