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EUTE 25C (EUTE W5), 27554

Orbit data source: Space-Track

EUTE 25C (EUTE W5), 27554 is a payload satellite owned by EutelsatSA (FR) in GEO that was launched on Wed, 20 Nov 2002 UTC via a DELTA 4M+(4,2) launch vehicle from the Air Force Eastern Test Range (AFETR). 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.

Not visible in the next 10 days
Identifier
27554, 2002-051A
Orbit
GEO
Country
Flag of FRFR / EUTE
Related business
Manufacturer
Alcatel/Cannes
Mission
Non-operational Commercial Communications
Bus & Motor
SPACEBUS 3000B2, S400
Mass
~3,170 kg wet, 1,285 kg dry
Launch date (UTC)
2002-11-20 (23 years ago)
Launch vehicle
DELTA 4M+(4,2)
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 14.5 m
Radar Cross Section
32.393 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 EUTE 25C (EUTE W5)
1 27554U 02051A   26101.07961308  .00000148  00000-0  00000-0 0  9998
2 27554   8.8197  60.6064 0014998 330.6670 226.0864  1.00217461 48121
Epoch: 2026-04-11T01:54Z
TLE epoch observation values (Epoch: 2026-04-11T01:54:38.570Z)
Latitude
-2.51201°
Longitude
29.08955°
Altitude
35,845.723 km
Speed
3.071 km/s
True Right ascension
17h 08m 13s
True Declination
-2° 30' 34"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
18:26:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,866.127 km
Perigee altitude
35,739.601 km
Semi-major axis
42,181.001 km
Eccentricity
0.0015
Inclination
8.8197°
RAAN
60.6064°
Arg. of periapsis
330.667°
True anomaly
225.96275°
Mean anomaly
226.0864°
Eccentric anomaly
226.02456°
Mean motion
0.25053 °/min
Orbital period
1,436.93 mins
BSTAR
0
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