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: 6 hours ago
TLE from 6 hours ago
0 EUTE 28A (EB 1)
1 26719U 01011A 26004.82820546 .00000050 00000-0 00000+0 0 9999
2 26719 6.9711 69.2193 0007595 256.6091 147.7576 0.98788708 90771Epoch: 2026-01-04T19:52Z
TLE epoch observation values (Epoch: 2026-01-04T19:52:36.951Z)
Latitude
4.90055°
Longitude
70.85043°
Altitude
36,234.069 km
Speed
3.058 km/s
True Right ascension
07h 33m 45s
True Declination
4° 53' 44"
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
01:36:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,240.93 km
Perigee altitude
36,176.241 km
Semi-major axis
42,586.722 km
Eccentricity
0.00076
Inclination
6.9711°
RAAN
69.2193°
Arg. of periapsis
256.6091°
True anomaly
147.80399°
Mean anomaly
147.7576°
Eccentric anomaly
147.7808°
Mean motion
0.24696 °/min
Orbital period
1,457.71 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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