GALILEO 10 (206), 40890
Orbit data source: Space-Track
GALILEO 10 (206), 40890 is a payload satellite owned by GNSS Agency (ESA) that was launched on Fri, 11 Sep 2015 UTC via a SOYUZ-ST-B 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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40890 intel report (Beta)
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Identifier
Orbit
Country
ESARelated business
Manufacturer
OHB
Mission
Operational Civil Navigation
Bus & Motor
GALILEOSAT, 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: 2 days ago
TLE from 2 days ago
0 GALILEO 10 (206)
1 40890U 15045B 26306.30478684 -.00000022 00000-0 00000-0 0 9998
2 40890 54.9081 217.7946 0003403 21.2477 338.8007 1.70472856 69395Epoch: 2026-11-02T07:18Z
TLE epoch observation values (Epoch: 2026-11-02T07:18:53.582Z)
Latitude
0.00002°
Longitude
66.48118°
Altitude
23,213.181 km
Speed
3.671 km/s
True Right ascension
14h 31m 09s
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
00:54:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
23,232.4 km
Perigee altitude
23,212.254 km
Semi-major axis
29,600.464 km
Eccentricity
0.00034
Inclination
54.9081°
RAAN
217.7946°
Arg. of periapsis
21.2477°
True anomaly
338.78659°
Mean anomaly
338.8007°
Eccentric anomaly
338.79365°
Mean motion
0.42618 °/min
Orbital period
844.71 mins
BSTAR
0
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Other satellites on launch #45 in the year 2015 (2015-09-11 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 10 (206) 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. |
|---|---|---|---|---|---|---|---|
| 278 mins | 2026-11-04 05:00:46.721Z | 312.627° NW | 2026-11-04 06:46:46.721Z | 272.636° WNW | 56.957° | 2026-11-04 09:38:46.721Z | 209.257° SW |
| 298 mins | 2026-11-04 14:59:46.721Z | 132.152° SE | 2026-11-04 17:28:46.721Z | 78.237° E | 43.236° | 2026-11-04 19:57:46.721Z | 42.728° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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