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, 14.5 m
Radar Cross Section
27.172 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 EUTE 28A (EB 1)
1 26719U 01011A 26015.80329262 -.00000114 00000-0 00000-0 0 9991
2 26719 6.9977 69.0991 0007766 263.8222 84.0056 0.98793822 90875Epoch: 2026-01-15T19:16Z
TLE epoch observation values (Epoch: 2026-01-15T19:16:44.482Z)
Latitude
-1.46076°
Longitude
12.67848°
Altitude
36,202.552 km
Speed
3.06 km/s
True Right ascension
03h 48m 27s
True Declination
-1° 27' 33"
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
09:16:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,240.187 km
Perigee altitude
36,174.044 km
Semi-major axis
42,585.253 km
Eccentricity
0.00078
Inclination
6.9977°
RAAN
69.0991°
Arg. of periapsis
263.8222°
True anomaly
84.09411°
Mean anomaly
84.0056°
Eccentric anomaly
84.04986°
Mean motion
0.24698 °/min
Orbital period
1,457.63 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
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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. |
|---|---|---|---|---|---|---|---|
| EUTE 28A (EB 1) is likely not visible in the next few days. |
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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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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