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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Identifier
Orbit
Country
FR / 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, 14.5 m
Radar Cross Section
27.172 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 EUTE 28A (EB 1)
1 26719U 01011A 26094.80836980 -.00000182 00000-0 00000-0 0 9993
2 26719 7.1987 68.1805 0008721 295.3435 72.1873 0.98793112 91666Epoch: 2026-04-04T19:24Z
TLE epoch observation values (Epoch: 2026-04-04T19:24:03.150Z)
Latitude
0.94584°
Longitude
-48.38473°
Altitude
36,194.207 km
Speed
3.06 km/s
True Right ascension
05h 03m 00s
True Declination
0° 56' 42"
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
09:54:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,244.457 km
Perigee altitude
36,170.18 km
Semi-major axis
42,585.455 km
Eccentricity
0.00087
Inclination
7.1987°
RAAN
68.1805°
Arg. of periapsis
295.3435°
True anomaly
72.28248°
Mean anomaly
72.1873°
Eccentric anomaly
72.23488°
Mean motion
0.24697 °/min
Orbital period
1,457.64 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 | 2026-04-05 04:00:35.182Z | 110.117° ESE | 2026-04-06 01:35:35.182Z | 112.35° ESE | 24.401° | 2026-04-06 04:00:35.182Z | 114.172° 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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