EUROBIRD 4A(EUTELSAT W1), 26487
Orbit data source: Space-Track
EUROBIRD 4A(EUTELSAT W1), 26487 is a payload satellite owned by Eutelsat (FR) in GEO that was launched on Wed, 06 Sep 2000 UTC via an ARIANE 44P 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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26487 intel report (Beta)
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Identifier
Orbit
Country
FR / EUTERelated business
Manufacturer
Astrium/Toulouse
Mission
Non-operational Civil Communications
Bus & Motor
EUROSTAR 2000+, R-4D-11-300
Mass
3,250 kg wet, 1,430 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 15.8 m
Radar Cross Section
35.202 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 EUROBIRD 4A(EUTELSAT W1)
1 26487U 00052A 26155.18239306 -.00000032 00000-0 00000-0 0 9991
2 26487 11.3114 46.1698 0010109 301.2171 246.3888 0.98179299 93050Epoch: 2026-06-04T04:22Z
TLE epoch observation values (Epoch: 2026-06-04T04:22:38.760Z)
Latitude
-1.48461°
Longitude
-84.75776°
Altitude
36,400.584 km
Speed
3.052 km/s
True Right ascension
15h 34m 08s
True Declination
-1° 28' 59"
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
08:23:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,427.814 km
Perigee altitude
36,341.357 km
Semi-major axis
42,762.722 km
Eccentricity
0.00101
Inclination
11.3114°
RAAN
46.1698°
Arg. of periapsis
301.2171°
True anomaly
246.28271°
Mean anomaly
246.3888°
Eccentric anomaly
246.33575°
Mean motion
0.24544 °/min
Orbital period
1,466.75 mins
BSTAR
0
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Other satellites on launch #52 in the year 2000 (2000-09-06 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.EUROBIRD 4A(EUTELSAT W1) 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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2026-06-05 22:26:40.008Z | 165.045° S | 2026-06-06 22:26:40.008Z | 180.506° SSW | 39.846° | 2026-06-06 22:26:40.008Z | 180.506° SSW |
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26487 neighbors
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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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