GALILEO 34 (139), 67162
Orbit data source: Space-Track
GALILEO 34 (139), 67162 is a payload satellite owned by EU SPA (ESA) that was launched on Wed, 17 Dec 2025 UTC via an ARIANE 62 launch vehicle from the French Guiana (FRGUI). 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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67162 intel report (Beta)
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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
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 GALILEO 34 (139)
1 67162U 25302C 26169.10704436 -.00000012 00000-0 00000-0 0 9997
2 67162 54.3376 102.1035 0002963 311.0872 230.0912 1.70473903 3190Epoch: 2026-06-18T02:34Z
TLE epoch observation values (Epoch: 2026-06-18T02:34:08.632Z)
Latitude
-0.99976°
Longitude
-22.07442°
Altitude
23,228.208 km
Speed
3.669 km/s
True Right ascension
18h 51m 16s
True Declination
0° 59' 54"
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
07:19:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
23,230.998 km
Perigee altitude
23,213.456 km
Semi-major axis
29,600.364 km
Eccentricity
0.0003
Inclination
54.3376°
RAAN
102.1035°
Arg. of periapsis
311.0872°
True anomaly
230.06516°
Mean anomaly
230.0912°
Eccentric anomaly
230.07818°
Mean motion
0.42618 °/min
Orbital period
844.7 mins
BSTAR
0
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Other satellites on launch #302 in the year 2025 (2025-12-17 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 34 (139) 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. |
|---|---|---|---|---|---|---|---|
| 136 mins | 2026-06-20 20:23:47.546Z | 62.173° ENE | 2026-06-20 20:23:47.546Z | 62.173° ENE | 37.699° | 2026-06-20 22:39:47.546Z | 51.74° ENE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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