GALILEO 22 (2C8), 43058
Orbit data source: Space-Track
GALILEO 22 (2C8), 43058 is a payload satellite owned by GNSS Agency (ESA) that was launched on Tue, 12 Dec 2017 UTC via an ARIANE 5ES 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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43058 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ESARelated business
Manufacturer
OHB
Mission
Operational Civil Navigation
Bus & Motor
GALILEOSAT, AOCS
Mass
715 kg wet, 700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 7.4 m
Radar Cross Section
9.223 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GALILEO 22 (2C8)
1 43058U 17079D 25258.05377801 .00000027 00000-0 00000-0 0 9996
2 43058 55.1633 229.0715 0005018 276.8701 83.0469 1.70473909 48323Epoch: 2025-09-15T01:17Z
TLE epoch observation values (Epoch: 2025-09-15T01:17:26.42Z)
Latitude
0.00007°
Longitude
-144.55972°
Altitude
23,220.676 km
Speed
3.67 km/s
True Right ascension
15h 16m 15s
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
00:52:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
23,237.05 km
Perigee altitude
23,207.343 km
Semi-major axis
29,600.333 km
Eccentricity
0.0005
Inclination
55.1633°
RAAN
229.0715°
Arg. of periapsis
276.8701°
True anomaly
83.10398°
Mean anomaly
83.0469°
Eccentric anomaly
83.07544°
Mean motion
0.42619 °/min
Orbital period
844.7 mins
BSTAR
0
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Other satellites on launch #79 in the year 2017 (2017-12-12 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 22 (2C8) 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. |
|---|---|---|---|---|---|---|---|
| 323 mins | 2025-09-16 08:10:40.020Z | 311.752° NW | 2025-09-16 10:41:40.020Z | 271.863° WNW | 40.215° | 2025-09-16 13:33:40.020Z | 208.557° SW |
| 294 mins | 2025-09-16 18:55:40.020Z | 131.056° SE | 2025-09-16 21:23:40.020Z | 77.366° E | 34.184° | 2025-09-16 23:49:40.020Z | 42.202° 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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