EUTE 28A (EB 1), 26719
Orbit data source: Space-Track
EUTE 28A (EB 1), 26719 is a payload satellite owned by Eutelsat (FR) in GEO that was launched on Thu, 08 Mar 2001 UTC via an ARIANE 5G 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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26719 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / EUTERelated business
Manufacturer
Alcatel/Cannes
Mission
Non-operational Commercial Communications
Bus & Motor
SPACEBUS 3000B2, S400
Mass
3,050 kg wet, ~1,300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.1 m
Radar Cross Section
27.172 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 EUTE 28A (EB 1)
1 26719U 01011A 25257.43269089 -.00000192 00000-0 00000-0 0 9993
2 26719 6.6823 70.4505 0002106 268.9972 119.8772 0.98792179 89661Epoch: 2025-09-14T10:23Z
TLE epoch observation values (Epoch: 2025-09-14T10:23:04.492Z)
Latitude
3.20756°
Longitude
-50.25246°
Altitude
36,210.177 km
Speed
3.059 km/s
True Right ascension
06h 36m 40s
True Declination
3° 12' 16"
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
01:03:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,216.558 km
Perigee altitude
36,198.621 km
Semi-major axis
42,585.727 km
Eccentricity
0.00021
Inclination
6.6823°
RAAN
70.4505°
Arg. of periapsis
268.9972°
True anomaly
119.89812°
Mean anomaly
119.8772°
Eccentric anomaly
119.88766°
Mean motion
0.24697 °/min
Orbital period
1,457.66 mins
BSTAR
0
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Other satellites on launch #11 in the year 2001 (2001-03-08 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.EUTE 28A (EB 1) 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 | 2025-09-15 08:25:27.098Z | 118.556° SE | 2025-09-15 15:09:27.098Z | 113.99° SE | 24.907° | 2025-09-16 08:25:27.098Z | 123.58° SE |
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26719 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
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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