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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Edit Public Description
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 25311.14175640 .00000004 00000-0 00000-0 0 9990
2 40890 55.0165 227.7366 0003132 22.5111 337.5426 1.70472821 63257Epoch: 2025-11-07T03:24Z
TLE epoch observation values (Epoch: 2025-11-07T03:24:07.752Z)
Latitude
-0.00002°
Longitude
130.10321°
Altitude
23,214.011 km
Speed
3.671 km/s
True Right ascension
15h 10m 54s
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
01:05:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
23,231.598 km
Perigee altitude
23,213.057 km
Semi-major axis
29,600.464 km
Eccentricity
0.00031
Inclination
55.0165°
RAAN
227.7366°
Arg. of periapsis
22.5111°
True anomaly
337.52889°
Mean anomaly
337.5426°
Eccentric anomaly
337.53574°
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. |
|---|---|---|---|---|---|---|---|
| 46 mins | 2025-11-09 04:51:15.791Z | 136.156° SSE | 2025-11-09 04:51:15.791Z | 136.156° SSE | 22.943° | 2025-11-09 05:37:15.791Z | 144.979° SSE |
| 50 mins | 2025-11-10 04:01:15.791Z | 308.451° NW | 2025-11-10 04:51:15.791Z | 312.957° NW | 23.352° | 2025-11-10 04:51:15.791Z | 312.957° NW |
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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